subject:(aerodynamik)

1. Thannan, Andreas. Utformining av vindavledare för flakkåpa.

Degree: Technology and Society, 2012, University of Skövde

URL: http://urn.kb.se/resolve?urn=urn:nbn:se:his:diva-6985

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På grund av nya EU-restriktioner måste biltillverkare sänka sina koldioxidutsläpp för att kunna konkurrera på marknaden. Denna rapport behandlar examensarbetet med att utveckla en vindavledare… (more)

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På grund av nya EU-restriktioner måste biltillverkare sänka sina koldioxidutsläpp för att kunna konkurrera på marknaden. Denna rapport behandlar examensarbetet med att utveckla en vindavledare för Autokaross i Floby AB’s flakkåpa monterad på en Volkswagen Transporter. Syftet är att, på grund av framtida EU restriktioner på max 175 CO₂/km för lätta transportfordon, sänka bränslekostnaderna och koldioxidutsläppet genom att minska luftmotståndet. En litteraturstudie kring hur aerodynamik fungerar gjordes och dagens marknad undersöktes för att se vilka lösningar som finns idag. Genom att ta del av en kundundersökning som Autokaross i Floby AB gjort kunde kundkrav identifieras vilka utgjorde grunden för kravspecifikationen. För att skaffa en stor kvantitet av idéer under konceptgenereringen utfördes brainstorming och brainwriting i omgångar. De olika idéerna utvecklades till koncept och genom konsultation med handledare på Autokaross kunde de mer intressanta koncepten väljas ut. Stor vikt har lagts på att göra analyser i CFD, Computitional Fluid Dynamics, där olika tvärsnitt har undersökts så väl som 3D-modeller för att se vilka former som har minst luftmotstånd. När slutkonceptet skulle väljas gjordes en konceptvalsmatris där resultaten från undersökningarna med hjälp av CFD-simuleringar hade störst påverkan. Resultatet blev två delar, en takspoiler och en boattail, som tillsammans med Autokaross redan befintliga sidokjol uppfyller målet med att sänka luftmotståndet och på så sätt CO₂-utsläppet och bränsleförbrukningen. Med dessa tre delar monterade sänks luftmotståndet med 27 procent.

Due to future EU-regulations, car manufacturers need to reduce their carbon dioxide emissions in order to compete with other companies. This report discusses the development of a wind deflector for Auto-kaross i Floby AB´s Ekobox mounted on a Volkswagen Transporter. The goal is to, due to future regulations of a maximum of 175 CO2/km for lightweight transport vehicles, reduce fuel costs and carbon diox-ide emissions by reducing air resistance. A study of aerodynamics and today’s market was made to find solutions applied to similar prob-lems. Through a costumer survey made by Autokaross, customer needs could be identified which formed the product specification. To gather a big amount of ideas during the concept generation several brainstorming methods were applied in sessions. The ideas were de-veloped into concepts and through consultations from the supervisor at Autokaross the most interesting concepts were picked out. The most important part in the project was the analysis in CFD, Computational Fluid Dynamics, where different cross sections were tested as well as full 3D-models to see what forms performs best and gets the lowest air resistance. When the final concept was to be chosen a concept selec-tion matrix was made were the results from the CFD-simulations had the biggest impact. The final result consists of two parts, a…

Subjects/Keywords: Aerodynamik

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APA (6^th Edition):

Thannan, A. (2012). Utformining av vindavledare för flakkåpa. (Thesis). University of Skövde. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:his:diva-6985

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Thannan, Andreas. “Utformining av vindavledare för flakkåpa.” 2012. Thesis, University of Skövde. Accessed February 28, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:his:diva-6985.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Thannan, Andreas. “Utformining av vindavledare för flakkåpa.” 2012. Web. 28 Feb 2021.

Vancouver:

Thannan A. Utformining av vindavledare för flakkåpa. [Internet] [Thesis]. University of Skövde; 2012. [cited 2021 Feb 28]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:his:diva-6985.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Thannan A. Utformining av vindavledare för flakkåpa. [Thesis]. University of Skövde; 2012. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:his:diva-6985

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Halmstad University

2. Edman, Fredrik. Aerodynamiskt fotstöd : Utveckling av individanpassat fotstöd för paracyklist.

Degree: Engineering and Science, 2016, Halmstad University

URL: http://urn.kb.se/resolve?urn=urn:nbn:se:hh:diva-31205

► This project has focused on aerodynamics in hand cycling. Hand cycles are used by people with disabilities, paralysis or amputation of a lower limb.… (more)

▼ This project has focused on aerodynamics in hand cycling. Hand cycles are used by people with disabilities, paralysis or amputation of a lower limb. The idea for the project was initiated by a para-cyclist who suspected that his feet were causing an unnecessarily large air resistance when racing. The aim of this project was therefore to investigate this suspicion. If the excessive air resistance was confirmed, a new footrest would be developed to reduce it. The project was conducted in collaboration with the orthopedic clinic Team Olmed who had previously had contact with the user. Simulations on the feet were carried out in FloEFD to investigate the air resistance caused by the feet. Any excessive air resistance could then be confirmed and the development of a new footrest that would reduce drag could begin. Through literature studies regarding aerodynamics and analogies, brainstorming and brainwriting and with help from experts different concepts were generated. The concept of a streamlined footrest served as a basis to reduce the air resistance. Two of the concepts were modeled with a rounded shape that gently breaks the air and forms a streamline along the body. New simulations were conducted and later compared with the old footrest and the new streamline characteristics could then be confirmed. The result of the post simulations cannot be definitively quantified, but they indicate that air resistance is reduced by about 0,3 N for the two new footrests. This represents an improvement of 12-15 seconds for the cyclist on a 20 km race, which could be crucial in future competitions. The concept that provided the lowest air resistance was also developed as a prototype. The prototype was tested on the user's bicycle and feet with a satisfactory result. The project shows that it is relevant to develop more aerodynamic footrests in the sport hand- cycling. The time saved with the footrest developed in this project had meant the difference between victory and a fourth place at the Paralympics in 2008.

Subjects/Keywords: Paracykling; Handcykling; Aerodynamik

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APA (6^th Edition):

Edman, F. (2016). Aerodynamiskt fotstöd : Utveckling av individanpassat fotstöd för paracyklist. (Thesis). Halmstad University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:hh:diva-31205

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Edman, Fredrik. “Aerodynamiskt fotstöd : Utveckling av individanpassat fotstöd för paracyklist.” 2016. Thesis, Halmstad University. Accessed February 28, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:hh:diva-31205.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Edman, Fredrik. “Aerodynamiskt fotstöd : Utveckling av individanpassat fotstöd för paracyklist.” 2016. Web. 28 Feb 2021.

Vancouver:

Edman F. Aerodynamiskt fotstöd : Utveckling av individanpassat fotstöd för paracyklist. [Internet] [Thesis]. Halmstad University; 2016. [cited 2021 Feb 28]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:hh:diva-31205.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Edman F. Aerodynamiskt fotstöd : Utveckling av individanpassat fotstöd för paracyklist. [Thesis]. Halmstad University; 2016. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:hh:diva-31205

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

3. Karvonen, Henrik. Exteriördesign av miljöbil.

Degree: Mathematics and Computer Science, 2007, University West

URL: http://urn.kb.se/resolve?urn=urn:nbn:se:hv:diva-777

► Sedan ett år tillbaka på företaget Elitkomposit AB pågår ett fordonsprojekt som syftar till att ta fram konstruktionsunderlag för en fyrhjulig miljöbil för två… (more)

Subjects/Keywords: Miljöbilar; Aerodynamik; Karosser; Kolfiber

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Karvonen, H. (2007). Exteriördesign av miljöbil. (Thesis). University West. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:hv:diva-777

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Karvonen, Henrik. “Exteriördesign av miljöbil.” 2007. Thesis, University West. Accessed February 28, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:hv:diva-777.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Karvonen, Henrik. “Exteriördesign av miljöbil.” 2007. Web. 28 Feb 2021.

Vancouver:

Karvonen H. Exteriördesign av miljöbil. [Internet] [Thesis]. University West; 2007. [cited 2021 Feb 28]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:hv:diva-777.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Karvonen H. Exteriördesign av miljöbil. [Thesis]. University West; 2007. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:hv:diva-777

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Jönköping University

4. Hansson, Richard. Konceptstudie av solcellsdriven bil.

Degree: Engineering, 2011, Jönköping University

URL: http://urn.kb.se/resolve?urn=urn:nbn:se:hj:diva-15547

► World Solar Challenge är en tävling i Australien vars syfte är att främja utvecklingen av förnyelsebar energi. Här deltar olika universitet runt om i… (more)

▼ World Solar Challenge är en tävling i Australien vars syfte är att främja utvecklingen av förnyelsebar energi. Här deltar olika universitet runt om i världen och för att bygga en solcellsdriven bil som drivs av solens energi. Den ska sedan köras en sträcka mellan Darwin och Adelaide på dryga 300 mil genom Australien på kortast möjligast tid. Projektet görs för Tekniska Högskolan i Jönköping till en kommande kurs som studenter kan söka sig till för att delta i World Solar Challenge 2013. I kursen ingår att bygga en solcellsbil som man sedan tävlar med. Genom att sätta upp krav som är nödvändiga och önskvärda i en funktionsanalys får projektet en utgångspunkt och ett stöd som bestämmer hur konceptet ska se ut och vilka krav som måste uppfyllas. De restriktioner som tävlingsledningen för World Solar Challenge upprättat kan omvandlas till nödvändiga krav i funktionsanalysen. Researchen, restriktionerna och de teorier som de aerodynamiska aspekterna pekat på bestämmer hur konceptet är utformat. Resultatet i projektet är en solcellsbil som med hjälp av sin sammanhängande form får goda aerodynamiska egenskaper och kan på det sättet konkurrera om en topplacering i World Solar Challenge. Konceptet kallas Sting och är ett trehjuligt fordon med en solcellsyta på 6m² som är den tillåtna ytan för kiselsolceller. Genom att placera förarhytten framtill påverkar inte luftmotståndet bakänden lika mycket, som är den del som utsätts för mest turbulens. Bakänden kan på detta sätt smalnas av och föra samman luftströmmarna igen utan att det uppstår turbulens. Designen av Sting kommer från fyra värdeord vilka är: snabb, miljövänlig, aerodynamisk och alternativa energikällor. Genom detta projekt kan konceptet utvecklas vidare i den kommande kursen hos Tekniska Högskolan i Jönköping . Slutsatsen är att konceptet uppfyller de krav som funktionsanalysen innehåller och att konceptet kan ligga till grund för kursen med en bra utgångspunkt.

Subjects/Keywords: Industri design; design; koncept; fordon; solcell; aerodynamik; skiss; examensarbete; richard hansson; TECHNOLOGY; TEKNIKVETENSKAP

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APA (6^th Edition):

Hansson, R. (2011). Konceptstudie av solcellsdriven bil. (Thesis). Jönköping University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:hj:diva-15547

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Hansson, Richard. “Konceptstudie av solcellsdriven bil.” 2011. Thesis, Jönköping University. Accessed February 28, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:hj:diva-15547.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Hansson, Richard. “Konceptstudie av solcellsdriven bil.” 2011. Web. 28 Feb 2021.

Vancouver:

Hansson R. Konceptstudie av solcellsdriven bil. [Internet] [Thesis]. Jönköping University; 2011. [cited 2021 Feb 28]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:hj:diva-15547.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Hansson R. Konceptstudie av solcellsdriven bil. [Thesis]. Jönköping University; 2011. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:hj:diva-15547

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

5. Weingarten, Helena. Aerodynamisk och historisk analys av bilen Type 64 .

Degree: Chalmers tekniska högskola / Institutionen för mekanik och maritima vetenskaper, 2020, Chalmers University of Technology

URL: http://hdl.handle.net/20.500.12380/300828

► Type 64 är en tävlingsbil som tillverkades av Ferdinand Porsche under 1930-talet, det är en bil med en gedigen och omtalad, men framförallt något oviss… (more)

▼ Type 64 är en tävlingsbil som tillverkades av Ferdinand Porsche under 1930-talet, det är en bil med en gedigen och omtalad, men framförallt något oviss historia. Bilen blev åter aktuell i augusti 2019 då en av de återstående bilarna lades ut till försäljning på en auktionsfirma, under benämningen Porsche Type 64, där framför allt Porschemärket skapade debatt. Eftersom det är en gammal bil som endast tillverkades i tre exemplar finns det inte någon information kring bilens aerodynamiska prestanda. Rapportens syfte är därför att genomföra simuleringar för att bestämma denna, samt reda ut dess historia. Med befintliga koordinater på bilen, analyserades dess aerodynamik med hjälp av Computational fluid dynamics. För att få en bättre förståelse över bilens beteende genomfördes simuleringarna i olika scenarier i form av varierande hastigheter, anströmningsvinklar (yaw-vinklar) samt fall med och utan hjulkåpor. Resultaten från simuleringarna gav värden på luftmotståndskoefficienten CD och lyftkraftskoefficienten CL, samt hur normalkraftsfördelningen på bilen förändrades. Resultaten analyserandes och tolkades tillsammans med figurer från simuleringarna, för att förstå resultatens innebörd. Från resultaten framgick det tydligt att bilens normalfördelning förskjuts framåt då hastigheten ökar, vilket gäller för samtliga fall vare sig det är med eller utan kåpor, eller med en förändrad anströmningsvinkel. Jämförelsen med och utan kåpor visade att då kåporna avlägsnats ökade både luftmotståndet och lyftkraften. Överlag är luftmotståndet relativt lågt och förändras inte nämnvärt mellan olika fall då hastigheten förändras, vilket är positivt ur ett designperspektiv. När det gäller lyftkraften sker störst förändring på bilens framaxel där beloppet ökade markant, vilket är den största anledningen till att normalfördelningen förskjuts framåt. Därmed är det denna faktor som har störst inverkan på bilens beteende och tenderar att göra den över- eller understyrd.

Subjects/Keywords: bil; aerodynamik; CFD-simulering; STAR-CCM+; Porsche; Type 64; lyftkraft; luftmotstånd; CL & CD; strömningsteori

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Weingarten, H. (2020). Aerodynamisk och historisk analys av bilen Type 64 . (Thesis). Chalmers University of Technology. Retrieved from http://hdl.handle.net/20.500.12380/300828

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Weingarten, Helena. “Aerodynamisk och historisk analys av bilen Type 64 .” 2020. Thesis, Chalmers University of Technology. Accessed February 28, 2021. http://hdl.handle.net/20.500.12380/300828.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Weingarten, Helena. “Aerodynamisk och historisk analys av bilen Type 64 .” 2020. Web. 28 Feb 2021.

Vancouver:

Weingarten H. Aerodynamisk och historisk analys av bilen Type 64 . [Internet] [Thesis]. Chalmers University of Technology; 2020. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/20.500.12380/300828.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Weingarten H. Aerodynamisk och historisk analys av bilen Type 64 . [Thesis]. Chalmers University of Technology; 2020. Available from: http://hdl.handle.net/20.500.12380/300828

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

6. Jain, Arnav. CFD beräkning på en jetmotorinstallation.

Degree: Design and Engineering, 2013, Mälardalen University

URL: http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-21746

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Hawk Turbine AB tillverkar mindre jetmotorer som ofta används i små obemannade och radiostyrda flygplan. I flygplansmodellen Lockheed T-33 Shooting Star är motorn monterad… (more)

Subjects/Keywords: Aerodynamik; Strömning; CFD; jet; jetmotor; motor

…atmosfärstrycket . Inom aerodynamik används ofta även en annan typ av tryck, total tryck. I Introduction… …Newtons andra lag antager en konstant massa, vilket innebär konstant volym. Men inom aerodynamik…

10 more images…

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Jain, A. (2013). CFD beräkning på en jetmotorinstallation. (Thesis). Mälardalen University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-21746

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Jain, Arnav. “CFD beräkning på en jetmotorinstallation.” 2013. Thesis, Mälardalen University. Accessed February 28, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-21746.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Jain, Arnav. “CFD beräkning på en jetmotorinstallation.” 2013. Web. 28 Feb 2021.

Vancouver:

Jain A. CFD beräkning på en jetmotorinstallation. [Internet] [Thesis]. Mälardalen University; 2013. [cited 2021 Feb 28]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-21746.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Jain A. CFD beräkning på en jetmotorinstallation. [Thesis]. Mälardalen University; 2013. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-21746

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Linköping University

7. Nordin, Erik. Development of Body and Viscous Contribution to a Panel Program for Potential Flow Computation : Aero Dynamic Analysis and Preliminary Design Tool.

Degree: Mechanical Engineering, 2006, Linköping University

URL: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-6111

► The aim of this thesis was to develop a potential flow calculation model which includes computation of flow around aircraft bodies (fuselage, engines) and… (more)

▼ The aim of this thesis was to develop a potential flow calculation model which includes computation of flow around aircraft bodies (fuselage, engines) and a boundary layer method which calculates the viscous effects over the aircraft wings. The models developed will be merged with an already existing panel program developed by Saab, Linköping, Sweden. Different methods have been studied but the basis of this work has been to develop a model using a panel method which can provide results from a simple geometry description, with short calculation time and hence be used in early design phases. In this thesis Matlab has been used as programming language, ensure that future development and maintenance is possible. The body model uses a panel method where the flow domain is divided into an inner and an outer part where the outer problem uses a three dimensional panel description while the inner problem performs two dimensional calculations. The inner and outer problems are separated by an arbitrarily shaped reference box. The inner area is divided into a number of cross sections which are described by line segments. With the help of these the two dimensional cross flow is obtained. This result is connected to the outer part through boundary conditions and the entire three dimensional flow domain can be determined. The resulting body program is limited to aircraft bodies with a slenderness ratio less than 1/5. Higher values violate the model assumption. The number of cross sections needed to describe a body of one unit length is between 80-150 and the number of line segments needed for one cross sections is 20 for the inner boundary and 40 line segments for the outer. This configuration gives results with acceptable accuracy within a computation time less than 15 seconds/body. The viscous effects around the aircraft wings are modelled with a two dimensional boundary layer model where the boundary layer displacement thickness over the wing profile is calculated with two different methods depending on if the flow in the boundary layer is laminar or turbulent. The computed displacement thickness is then added to the wing profile geometry and new pressure distributions are computed on the modified geometry. The computed pressure distributions including the viscous effects show better agreement with results from experimental wind tunnel tests than the inviscid without boundary layer contribution. Separation is not modelled and neither are the large effects this has on the pressure distribution. The model gives usable results up to 15-20 degrees angle of attack; at higher angles the separated regions are so large that the model is not valid anyway. The work was performed at the Department of Applied Aerodynamics and Flight Mechanics at Saab Aerosystems during the period 2005-08-24 – 2006-01-31.

Subjects/Keywords: Flygteknik; Aerodynamik; Potentiellströmning; Panelprogram; Kroppsmodell; Gränsskiktsmodell; TECHNOLOGY; TEKNIKVETENSKAP

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Nordin, E. (2006). Development of Body and Viscous Contribution to a Panel Program for Potential Flow Computation : Aero Dynamic Analysis and Preliminary Design Tool. (Thesis). Linköping University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-6111

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Nordin, Erik. “Development of Body and Viscous Contribution to a Panel Program for Potential Flow Computation : Aero Dynamic Analysis and Preliminary Design Tool.” 2006. Thesis, Linköping University. Accessed February 28, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-6111.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Nordin, Erik. “Development of Body and Viscous Contribution to a Panel Program for Potential Flow Computation : Aero Dynamic Analysis and Preliminary Design Tool.” 2006. Web. 28 Feb 2021.

Vancouver:

Nordin E. Development of Body and Viscous Contribution to a Panel Program for Potential Flow Computation : Aero Dynamic Analysis and Preliminary Design Tool. [Internet] [Thesis]. Linköping University; 2006. [cited 2021 Feb 28]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-6111.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Nordin E. Development of Body and Viscous Contribution to a Panel Program for Potential Flow Computation : Aero Dynamic Analysis and Preliminary Design Tool. [Thesis]. Linköping University; 2006. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-6111

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

8. Hemmingsson, Daniel. Reglerbar kylartäckning - En lösning till isbildningsproblematik i laddluftkylaren.

Degree: Design and Engineering, 2015, Mälardalen University

URL: http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-28463

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Denna rapport ingår i ett examensarbete på avancerad nivå inom ämnet produktutveckling.Arbetet innefattar en fallstudie som genomförts vid RTGA, Scania CV AB i Södertälje.Examensarbetet… (more)

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Denna rapport ingår i ett examensarbete på avancerad nivå inom ämnet produktutveckling.Arbetet innefattar en fallstudie som genomförts vid RTGA, Scania CV AB i Södertälje.Examensarbetet omfattar 30 högskolepoäng och har genomförts av undertecknad,teknologstudent från Mälardalens Högskola vårterminen 2015. Rapporten har upprättats i tvåversioner, en för Scania CV AB respektive en generell version där känslig företagsspecifikinformation har censurerats. I takt med att utvecklingen av motorprestanda fortskrider, med avseende på ökademotoreffekter samt teknikutveckling för emissionsreglering, så ökar också kravet på prestandaför kylsystem som måste klara av att kyla bort högre effekter. Fordonskombinationer medkraftfulla laddluftkylare löper dock stor risk att drabbas av utfälld kondens som fryser till is iladdluftkylaren vid låga omgivningstemperaturer. Isen medför ett tryckfall i laddluftkylarenmed prestandabortfall som följd. Scanias lösning till problematiken är en så kallad kylargardinsom syftar till att reducera kylluftflödet genom laddluftkylaren till den mån att isbildning intesker. Kylargardinen monteras manuellt av föraren framför kylarpaketet dåomgivningstemperaturen understiger 5 °C. Det finns även andra fördelar med att begränsa det yttre kylluftflödet som passerar genomkylarpaketet. Lastbilars kylsystem är i regel överdimensionerade för normala driftfall såsommotorvägskörning vilket betyder att maximal kylning inte krävs vid dessa situationer. Genomatt reducera det yttre kylluftflödet genom kylarpaketet så kan även hela fordonets totalaluftmotstånd reduceras vilket kan utnyttjas i syfte att reducera bränsleförbrukningen. För att erhålla en bra balansgång mellan aerodynamik och kylprestanda samt motverkaproblemet med isbildning i laddluftkylaren fanns därför en önskan om att en reglerbarkylartäckning skulle utvecklas för att kunna reglera kylluftflödet genom fordonets kylarpaketvid behov. Detta arbete innefattar en fallstudie där olika produktutvecklingsverktyg använts för att ta framolika konceptlösningar, anpassade för en specifik lastbil. Datorstödda flödessimuleringarutnyttjas för att utvärdera respektive verifiera konceptens funktion jämfört med olika referensmodeller. Resultatet visar bland annat att det slutgiltiga konceptets funktionsduglighet överensstämmermed den lösning som används idag samt att kylluftflödet inte påverkas nämnvärt då maximalkylkapacitet eftersträvas. Resultatet från den aerodynamiska flödessimuleringen indikerar ävenatt fordonets totala luftmotstånd kan reduceras med - Drag Counts (DC) vid hastigheten90 km/h och 0° vindriktning. Detta medför att bränsleförbrukningen i det specifika driftfallet,enligt tumregel, antas reduceras med - % för det specifika fordonet.

This report is part of a Master thesis project in the subject of Product Development. The workincludes a case study which was carried out at RTGA, Scania CV AB in Södertälje. The workcomprises 30 credits and was conducted by a student from Mälardalen University during thespring…

Subjects/Keywords: Charge Air Cooler; Ice build-up; Condensation; Truck; CFD; Drag reduction; Aerodynamics; Laddluftkylare; Kondens; Isbildning; Lastbil; CFD; Luftmotstånd; Aerodynamik

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Hemmingsson, D. (2015). Reglerbar kylartäckning - En lösning till isbildningsproblematik i laddluftkylaren. (Thesis). Mälardalen University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-28463

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Hemmingsson, Daniel. “Reglerbar kylartäckning - En lösning till isbildningsproblematik i laddluftkylaren.” 2015. Thesis, Mälardalen University. Accessed February 28, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-28463.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Hemmingsson, Daniel. “Reglerbar kylartäckning - En lösning till isbildningsproblematik i laddluftkylaren.” 2015. Web. 28 Feb 2021.

Vancouver:

Hemmingsson D. Reglerbar kylartäckning - En lösning till isbildningsproblematik i laddluftkylaren. [Internet] [Thesis]. Mälardalen University; 2015. [cited 2021 Feb 28]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-28463.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Hemmingsson D. Reglerbar kylartäckning - En lösning till isbildningsproblematik i laddluftkylaren. [Thesis]. Mälardalen University; 2015. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-28463

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

KTH

9. Mallor, Fermin. Enabling high-fidelity measurements of turbulent boundary layer flow over wing sections in the MTL wind tunnel.

Degree: Mechanics, 2019, KTH

URL: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-264842

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A reinforced fiber-glass model of a NACA 4412 wing profile is designed and set-up in the Minimum Turbulence Level (MTL) wind tunnel facility at… (more)

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A reinforced fiber-glass model of a NACA 4412 wing profile is designed and set-up in the Minimum Turbulence Level (MTL) wind tunnel facility at KTH. The model has 65 pressure taps orifices, and the set-up includes two mounting panels designed to allow for particle image velocimetry (PIV) and hot wire anemometry (HWA) measurements of the boundary layer (to be performed in a future campaign). In a first experimental campaign pressure scans are conducted at three angles of attack of interest (5,10 and 12 degrees), and at four different Reynolds numbers based on chord length and inflow velocity (200,000, 400,000, 1,000,000, and 1,640,000). The preliminary results show good agreement with DNS and LES data, however, the effective angle of attack of the wing is affected by the interference of the test section. In order to obtain proper flow conditions for future campaigns inside the test section, wall inserts are designed using 2D k-omega SST simulations. The side-walls are streamlined and the final geometry is corrected to account for the boundary-layer growth over them. The inserts are shown to avoid early separation near the trailing edge at higher angles of attack (10 and 12 degrees), but the 2D simulations fail to capture the aforementioned angle-of-attack issue affecting the pressure distributions. Future extensions of the present insert design should include both 3D simulations of the test-section and a robust optimization procedure to prescribe the resulting pressure distribution.

En NACA 4412 vingprofilsmodel av förstärkt glasfiber utformas och installeras enligt Minimum Turbulence Level (MTL) i vindtunnelanläggningen på KTH. Modellen har 65 tryckluftsöppningar, och uppsättningen innehåller två monteringspaneler som är utformade för att möjliggöra mätningar av particle image velocimetry (PIV) and hot wire anemometry (HWA) hos gränsskiktet (som ska utföras i en framtida kampanj). I en första experimentell kampanj utförs tryckskanningar vid tre anfallsvinklar av intresse (5, 10, och 12 grader) samt vid fyra olika Reynolds-nummer (200 000, 400 000, 1 000 000 och 1 640 000). De preliminära resultaten visar god överensstämmelse med DNS- och LES-data, men den effektiva anfallsvinkeln på vingen påverkas av störningar från testsektionen. För att tillhandahålla korrekta flödesförhållanden för framtida kampanjer i testdelen är vägginsatser konstruerade med 2D k-omega SST-simuleringar. Sidoväggarna är strömlinjeformade och den slutliga geometrin korrigeras för att ta hänsyn till gränsiktets tillväxt. Insatserna undviker den tidig separation som sker nära bakkanten vid högre anfallsvinklar (10 och 12 grader), men 2D-simuleringarna misslyckades med att fånga det ovan nämnda anfallsvinkelproblemet som påverkar tryckfördelningarna.

Subjects/Keywords: Fluid mechanics; aerodynamics; turbulence; RANS; wind-tunnel experiments; insert design; Strömningsmekanik; aerodynamik; turbulens; RANS; vindtunnel experiment; inlaga designen; Mechanical Engineering; Maskinteknik

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Mallor, F. (2019). Enabling high-fidelity measurements of turbulent boundary layer flow over wing sections in the MTL wind tunnel. (Thesis). KTH. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-264842

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Mallor, Fermin. “Enabling high-fidelity measurements of turbulent boundary layer flow over wing sections in the MTL wind tunnel.” 2019. Thesis, KTH. Accessed February 28, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-264842.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Mallor, Fermin. “Enabling high-fidelity measurements of turbulent boundary layer flow over wing sections in the MTL wind tunnel.” 2019. Web. 28 Feb 2021.

Vancouver:

Mallor F. Enabling high-fidelity measurements of turbulent boundary layer flow over wing sections in the MTL wind tunnel. [Internet] [Thesis]. KTH; 2019. [cited 2021 Feb 28]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-264842.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Mallor F. Enabling high-fidelity measurements of turbulent boundary layer flow over wing sections in the MTL wind tunnel. [Thesis]. KTH; 2019. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-264842

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

10. Sedlak, Vojtech. Motorcycle Cornering Improvement : An Aerodynamical Approach based on Flow Interference.

Degree: Mechanics, 2012, KTHKTH

URL: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-131200

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A new aerodynamic device, based on flow interference effects, is studied in order to significantly improve the cornering performance of racing motorcycles in MotoGP.… (more)

Subjects/Keywords: aerodynamic; fluid mechanics; interference; blockage; airfoil; wing; bluff body; motorcycle; moto; motorbike; MotoGP; road racing; aerodynamik; fluid mekanik; flöde interferenser; vinge; motorcyckel; MotoGP; roadracing

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Sedlak, V. (2012). Motorcycle Cornering Improvement : An Aerodynamical Approach based on Flow Interference. (Thesis). KTHKTH. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-131200

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Sedlak, Vojtech. “Motorcycle Cornering Improvement : An Aerodynamical Approach based on Flow Interference.” 2012. Thesis, KTHKTH. Accessed February 28, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-131200.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Sedlak, Vojtech. “Motorcycle Cornering Improvement : An Aerodynamical Approach based on Flow Interference.” 2012. Web. 28 Feb 2021.

Vancouver:

Sedlak V. Motorcycle Cornering Improvement : An Aerodynamical Approach based on Flow Interference. [Internet] [Thesis]. KTHKTH; 2012. [cited 2021 Feb 28]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-131200.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Sedlak V. Motorcycle Cornering Improvement : An Aerodynamical Approach based on Flow Interference. [Thesis]. KTHKTH; 2012. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-131200

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

ETH Zürich

11. Ryan, Lloyd Frederick. Experiments on aerodynamic cooling.

Degree: 1951, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/133499

Subjects/Keywords: LUFTWIDERSTAND (AERODYNAMIK); AIR RESISTANCE (AERODYNAMICS); info:eu-repo/classification/ddc/530; Physics

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Ryan, L. F. (1951). Experiments on aerodynamic cooling. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/133499

Chicago Manual of Style (16^th Edition):

Ryan, Lloyd Frederick. “Experiments on aerodynamic cooling.” 1951. Doctoral Dissertation, ETH Zürich. Accessed February 28, 2021. http://hdl.handle.net/20.500.11850/133499.

MLA Handbook (7^th Edition):

Ryan, Lloyd Frederick. “Experiments on aerodynamic cooling.” 1951. Web. 28 Feb 2021.

Vancouver:

Ryan LF. Experiments on aerodynamic cooling. [Internet] [Doctoral dissertation]. ETH Zürich; 1951. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/20.500.11850/133499.

Council of Science Editors:

Ryan LF. Experiments on aerodynamic cooling. [Doctoral Dissertation]. ETH Zürich; 1951. Available from: http://hdl.handle.net/20.500.11850/133499

ETH Zürich

12. Studer, Hans-Luzi. Experimentelle Untersuchungen über Flügelschwingungen.

Degree: 1936, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/135424

Subjects/Keywords: TRAGFLÜGELCHARAKTERISTIK (AERODYNAMIK); FLATTERN (AERODYNAMIK); AEROFOIL CHARACTERISTICS (AERODYNAMICS); FLUTTER (AERODYNAMICS); info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/530; Engineering & allied operations; Physics

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Studer, H. (1936). Experimentelle Untersuchungen über Flügelschwingungen. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/135424

Chicago Manual of Style (16^th Edition):

Studer, Hans-Luzi. “Experimentelle Untersuchungen über Flügelschwingungen.” 1936. Doctoral Dissertation, ETH Zürich. Accessed February 28, 2021. http://hdl.handle.net/20.500.11850/135424.

MLA Handbook (7^th Edition):

Studer, Hans-Luzi. “Experimentelle Untersuchungen über Flügelschwingungen.” 1936. Web. 28 Feb 2021.

Vancouver:

Studer H. Experimentelle Untersuchungen über Flügelschwingungen. [Internet] [Doctoral dissertation]. ETH Zürich; 1936. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/20.500.11850/135424.

Council of Science Editors:

Studer H. Experimentelle Untersuchungen über Flügelschwingungen. [Doctoral Dissertation]. ETH Zürich; 1936. Available from: http://hdl.handle.net/20.500.11850/135424

ETH Zürich

13. Dätwyler, Gottfried. Untersuchungen über das Verhalten von Tragflügelprofilen sehr nahe am Boden.

Degree: 1934, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/133416

Subjects/Keywords: TRAGFLÄCHEN, TRAGFLÄCHENUMRISSE (AERODYNAMIK); AERODYNAMIK VON FAHRZEUGEN; COMPLETE WINGS, PLANFORMS (AERODYNAMICS); AERODYNAMICS OF VEHICLES; info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/530; Engineering & allied operations; Physics

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Dätwyler, G. (1934). Untersuchungen über das Verhalten von Tragflügelprofilen sehr nahe am Boden. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/133416

Chicago Manual of Style (16^th Edition):

Dätwyler, Gottfried. “Untersuchungen über das Verhalten von Tragflügelprofilen sehr nahe am Boden.” 1934. Doctoral Dissertation, ETH Zürich. Accessed February 28, 2021. http://hdl.handle.net/20.500.11850/133416.

MLA Handbook (7^th Edition):

Dätwyler, Gottfried. “Untersuchungen über das Verhalten von Tragflügelprofilen sehr nahe am Boden.” 1934. Web. 28 Feb 2021.

Vancouver:

Dätwyler G. Untersuchungen über das Verhalten von Tragflügelprofilen sehr nahe am Boden. [Internet] [Doctoral dissertation]. ETH Zürich; 1934. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/20.500.11850/133416.

Council of Science Editors:

Dätwyler G. Untersuchungen über das Verhalten von Tragflügelprofilen sehr nahe am Boden. [Doctoral Dissertation]. ETH Zürich; 1934. Available from: http://hdl.handle.net/20.500.11850/133416

ETH Zürich

14. Feddersen, Berend. Wind tunnel modelling of turbulence and dispersion above tall and highly dense urgan roughness.

Degree: 2005, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/64109

Subjects/Keywords: TURBULENTE GRENZSCHICHTEN (FLUIDDYNAMIK); WINDKANÄLE, TESTS, MODELLVERSUCHE (AERODYNAMIK); TURBULENT BOUNDARY LAYERS (FLUID DYNAMICS); TURBULENT PIPE FLOW (FLUID DYNAMICS); AERODYNAMIK DER BAUWERKE (AERODYNAMIK); AERODYNAMICS OF BUILDINGS (AERODYNAMICS); WIND TUNNELS, TESTING, MODEL STUDIES (AERODYNAMICS); TURBULENTE STRÖMUNG IN RÖHREN (FLUIDDYNAMIK); info:eu-repo/classification/ddc/690; Buildings

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Feddersen, B. (2005). Wind tunnel modelling of turbulence and dispersion above tall and highly dense urgan roughness. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/64109

Chicago Manual of Style (16^th Edition):

Feddersen, Berend. “Wind tunnel modelling of turbulence and dispersion above tall and highly dense urgan roughness.” 2005. Doctoral Dissertation, ETH Zürich. Accessed February 28, 2021. http://hdl.handle.net/20.500.11850/64109.

MLA Handbook (7^th Edition):

Feddersen, Berend. “Wind tunnel modelling of turbulence and dispersion above tall and highly dense urgan roughness.” 2005. Web. 28 Feb 2021.

Vancouver:

Feddersen B. Wind tunnel modelling of turbulence and dispersion above tall and highly dense urgan roughness. [Internet] [Doctoral dissertation]. ETH Zürich; 2005. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/20.500.11850/64109.

Council of Science Editors:

Feddersen B. Wind tunnel modelling of turbulence and dispersion above tall and highly dense urgan roughness. [Doctoral Dissertation]. ETH Zürich; 2005. Available from: http://hdl.handle.net/20.500.11850/64109

ETH Zürich

15. Jenny, Philipp. Interaction mechanisms between rim seal purge flow and profiled end walls in a low-pressure turbine.

Degree: 2012, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/63223

Subjects/Keywords: SCOOPS, BLADES (INTERNAL AERODYNAMICS); ROTORS, IMPELLERS (TURBOMACHINES); KÜHLUNG DURCH LUFT ODER GASE (MASCHINENBAU); COOLING BY AIR OR GAS (MECHANICAL ENGINEERING); SCHAUFELN (INNERE AERODYNAMIK); INNERE AERODYNAMIK (AERODYNAMIK); TURBOMASCHINEN (MASCHINENBAU); ROTOREN, LAUFRÄDER (TURBOMASCHINEN); TURBOMACHINES (MECHANICAL ENGINEERING); WELLENDICHTUNGEN (MASCHINENELEMENTE); SHAFT SEALINGS (MACHINE COMPONENTS); INTERNAL AERODYNAMICS (AERODYNAMICS); info:eu-repo/classification/ddc/620; Engineering & allied operations

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Jenny, P. (2012). Interaction mechanisms between rim seal purge flow and profiled end walls in a low-pressure turbine. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/63223

Chicago Manual of Style (16^th Edition):

Jenny, Philipp. “Interaction mechanisms between rim seal purge flow and profiled end walls in a low-pressure turbine.” 2012. Doctoral Dissertation, ETH Zürich. Accessed February 28, 2021. http://hdl.handle.net/20.500.11850/63223.

MLA Handbook (7^th Edition):

Jenny, Philipp. “Interaction mechanisms between rim seal purge flow and profiled end walls in a low-pressure turbine.” 2012. Web. 28 Feb 2021.

Vancouver:

Jenny P. Interaction mechanisms between rim seal purge flow and profiled end walls in a low-pressure turbine. [Internet] [Doctoral dissertation]. ETH Zürich; 2012. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/20.500.11850/63223.

Council of Science Editors:

Jenny P. Interaction mechanisms between rim seal purge flow and profiled end walls in a low-pressure turbine. [Doctoral Dissertation]. ETH Zürich; 2012. Available from: http://hdl.handle.net/20.500.11850/63223

ETH Zürich

16. Barmpalias, Konstantinos G. Steam turbine aerodynamics and geometry optimization for effective reduction of leakage flow interactions.

Degree: 2011, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/44279

Subjects/Keywords: SCOOPS, BLADES (INTERNAL AERODYNAMICS); AXIALTURBOMASCHINEN (MASCHINENBAU); SCHAUFELN (INNERE AERODYNAMIK); STEAM TURBINES (HEAT ENGINES); INNERE AERODYNAMIK (AERODYNAMIK); LABYRINTH SEALS (MACHINE COMPONENTS); AXIAL TURBOMACHINES (MECHANICAL ENGINEERING); LABYRINTHDICHTUNGEN (MASCHINENELEMENTE); INTERNAL AERODYNAMICS (AERODYNAMICS); DAMPFTURBINEN (WÄRMEKRAFTMASCHINEN); info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/530; Engineering & allied operations; Physics

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Barmpalias, K. G. (2011). Steam turbine aerodynamics and geometry optimization for effective reduction of leakage flow interactions. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/44279

Chicago Manual of Style (16^th Edition):

Barmpalias, Konstantinos G. “Steam turbine aerodynamics and geometry optimization for effective reduction of leakage flow interactions.” 2011. Doctoral Dissertation, ETH Zürich. Accessed February 28, 2021. http://hdl.handle.net/20.500.11850/44279.

MLA Handbook (7^th Edition):

Barmpalias, Konstantinos G. “Steam turbine aerodynamics and geometry optimization for effective reduction of leakage flow interactions.” 2011. Web. 28 Feb 2021.

Vancouver:

Barmpalias KG. Steam turbine aerodynamics and geometry optimization for effective reduction of leakage flow interactions. [Internet] [Doctoral dissertation]. ETH Zürich; 2011. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/20.500.11850/44279.

Council of Science Editors:

Barmpalias KG. Steam turbine aerodynamics and geometry optimization for effective reduction of leakage flow interactions. [Doctoral Dissertation]. ETH Zürich; 2011. Available from: http://hdl.handle.net/20.500.11850/44279

ETH Zürich

17. Pfenninger, Werner. Untersuchungen über Reibungsverminderungen an Tragflügeln: insbesondere mit Hilfe von Grenzschichtabsaugung.

Degree: 1946, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/134570

Subjects/Keywords: TRAGFLÜGELCHARAKTERISTIK (AERODYNAMIK); GRENZSCHICHTABSAUGUNG + GRENZSCHICHTAUSBLASUNG (AERODYNAMIK); LUFTWIDERSTAND DURCH OBERFLÄCHENREIBUNG (AERODYNAMIK); AEROFOIL CHARACTERISTICS (AERODYNAMICS); BOUNDARY LAYER SUCTION + BOUNDARY LAYER BLOWING (AERODYNAMICS); AIR RESISTANCE DUE TO SURFACE FRICTION (AERODYNAMICS); info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/530; Engineering & allied operations; Physics

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Pfenninger, W. (1946). Untersuchungen über Reibungsverminderungen an Tragflügeln: insbesondere mit Hilfe von Grenzschichtabsaugung. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/134570

Chicago Manual of Style (16^th Edition):

Pfenninger, Werner. “Untersuchungen über Reibungsverminderungen an Tragflügeln: insbesondere mit Hilfe von Grenzschichtabsaugung.” 1946. Doctoral Dissertation, ETH Zürich. Accessed February 28, 2021. http://hdl.handle.net/20.500.11850/134570.

MLA Handbook (7^th Edition):

Pfenninger, Werner. “Untersuchungen über Reibungsverminderungen an Tragflügeln: insbesondere mit Hilfe von Grenzschichtabsaugung.” 1946. Web. 28 Feb 2021.

Vancouver:

Pfenninger W. Untersuchungen über Reibungsverminderungen an Tragflügeln: insbesondere mit Hilfe von Grenzschichtabsaugung. [Internet] [Doctoral dissertation]. ETH Zürich; 1946. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/20.500.11850/134570.

Council of Science Editors:

Pfenninger W. Untersuchungen über Reibungsverminderungen an Tragflügeln: insbesondere mit Hilfe von Grenzschichtabsaugung. [Doctoral Dissertation]. ETH Zürich; 1946. Available from: http://hdl.handle.net/20.500.11850/134570

ETH Zürich

18. Paterna, Enrico. Wind Tunnel Investigation of Turbulent Flow in Urban Configurations: A Time-Resolved PIV Analysis.

Degree: 2015, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/112286

Subjects/Keywords: TURBULENTE STRÖMUNG (FLUIDDYNAMIK); WINDKANÄLE, TESTS, MODELLVERSUCHE (AERODYNAMIK); AERODYNAMIK DER BAUWERKE (AERODYNAMIK); AERODYNAMICS OF BUILDINGS (AERODYNAMICS); TURBULENT FLOW (FLUID DYNAMICS); WIND TUNNELS, TESTING, MODEL STUDIES (AERODYNAMICS); info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/530; Engineering & allied operations; Physics

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APA (6^th Edition):

Paterna, E. (2015). Wind Tunnel Investigation of Turbulent Flow in Urban Configurations: A Time-Resolved PIV Analysis. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/112286

Chicago Manual of Style (16^th Edition):

Paterna, Enrico. “Wind Tunnel Investigation of Turbulent Flow in Urban Configurations: A Time-Resolved PIV Analysis.” 2015. Doctoral Dissertation, ETH Zürich. Accessed February 28, 2021. http://hdl.handle.net/20.500.11850/112286.

MLA Handbook (7^th Edition):

Paterna, Enrico. “Wind Tunnel Investigation of Turbulent Flow in Urban Configurations: A Time-Resolved PIV Analysis.” 2015. Web. 28 Feb 2021.

Vancouver:

Paterna E. Wind Tunnel Investigation of Turbulent Flow in Urban Configurations: A Time-Resolved PIV Analysis. [Internet] [Doctoral dissertation]. ETH Zürich; 2015. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/20.500.11850/112286.

Council of Science Editors:

Paterna E. Wind Tunnel Investigation of Turbulent Flow in Urban Configurations: A Time-Resolved PIV Analysis. [Doctoral Dissertation]. ETH Zürich; 2015. Available from: http://hdl.handle.net/20.500.11850/112286

ETH Zürich

19. Regina, Kai. High-Pressure Turbines with Novel Airfoils and End Walls Operating under Engine Representative Aero-Thermodynamic Effects.

Degree: 2015, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/155299

Subjects/Keywords: TURBOMASCHINENSCHAUFELN (TURBOMASCHINEN); INNERE AERODYNAMIK (AERODYNAMIK); COMPUTATIONAL FLUID DYNAMICS (FLUIDMECHANIK); TURBOMACHINE BLADES (TURBOMACHINES); INTERNAL AERODYNAMICS (AERODYNAMICS); COMPUTATIONAL FLUID DYNAMICS (FLUID MECHANICS); info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/530; Engineering & allied operations; Physics

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APA (6^th Edition):

Regina, K. (2015). High-Pressure Turbines with Novel Airfoils and End Walls Operating under Engine Representative Aero-Thermodynamic Effects. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/155299

Chicago Manual of Style (16^th Edition):

Regina, Kai. “High-Pressure Turbines with Novel Airfoils and End Walls Operating under Engine Representative Aero-Thermodynamic Effects.” 2015. Doctoral Dissertation, ETH Zürich. Accessed February 28, 2021. http://hdl.handle.net/20.500.11850/155299.

MLA Handbook (7^th Edition):

Regina, Kai. “High-Pressure Turbines with Novel Airfoils and End Walls Operating under Engine Representative Aero-Thermodynamic Effects.” 2015. Web. 28 Feb 2021.

Vancouver:

Regina K. High-Pressure Turbines with Novel Airfoils and End Walls Operating under Engine Representative Aero-Thermodynamic Effects. [Internet] [Doctoral dissertation]. ETH Zürich; 2015. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/20.500.11850/155299.

Council of Science Editors:

Regina K. High-Pressure Turbines with Novel Airfoils and End Walls Operating under Engine Representative Aero-Thermodynamic Effects. [Doctoral Dissertation]. ETH Zürich; 2015. Available from: http://hdl.handle.net/20.500.11850/155299

ETH Zürich

20. Bazjanac, Davorin. Untersuchungen mit Hilfe der elektrischen Analogie über den Einfluss der Luftstrahlbegrenzung in Windkanälen auf Tragflügelmessungen.

Degree: 1943, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/135681

Subjects/Keywords: TRAGFLÄCHENKONSTRUKTION UND DIMENSIONSCHARAKTERISTIKEN (AERODYNAMIK); LUFTSTRÖMUNGS-VARIABLE (AERODYNAMIK); AIRFOIL DESIGN AND DIMENSIONAL CHARACTERISTICS (AERODYNAMICS); AIR-FLOW VARIABLES (AERODYNAMICS); info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/530; Engineering & allied operations; Physics

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APA (6^th Edition):

Bazjanac, D. (1943). Untersuchungen mit Hilfe der elektrischen Analogie über den Einfluss der Luftstrahlbegrenzung in Windkanälen auf Tragflügelmessungen. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/135681

Chicago Manual of Style (16^th Edition):

Bazjanac, Davorin. “Untersuchungen mit Hilfe der elektrischen Analogie über den Einfluss der Luftstrahlbegrenzung in Windkanälen auf Tragflügelmessungen.” 1943. Doctoral Dissertation, ETH Zürich. Accessed February 28, 2021. http://hdl.handle.net/20.500.11850/135681.

MLA Handbook (7^th Edition):

Bazjanac, Davorin. “Untersuchungen mit Hilfe der elektrischen Analogie über den Einfluss der Luftstrahlbegrenzung in Windkanälen auf Tragflügelmessungen.” 1943. Web. 28 Feb 2021.

Vancouver:

Bazjanac D. Untersuchungen mit Hilfe der elektrischen Analogie über den Einfluss der Luftstrahlbegrenzung in Windkanälen auf Tragflügelmessungen. [Internet] [Doctoral dissertation]. ETH Zürich; 1943. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/20.500.11850/135681.

Council of Science Editors:

Bazjanac D. Untersuchungen mit Hilfe der elektrischen Analogie über den Einfluss der Luftstrahlbegrenzung in Windkanälen auf Tragflügelmessungen. [Doctoral Dissertation]. ETH Zürich; 1943. Available from: http://hdl.handle.net/20.500.11850/135681

ETH Zürich

21. Immer, Marc Christian. Time-resolved measurement and simulation of local scale turbulent urban flow.

Degree: 2016, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/112287

Subjects/Keywords: WINDKANÄLE, TESTS, MODELLVERSUCHE (AERODYNAMIK); AERODYNAMIK; WIND TUNNELS, TESTING, MODEL STUDIES (AERODYNAMICS); STADTPLANUNG + STÄDTEBAU (GEBAUTE UMWELT); URBAN PLANNING (BUILT ENVIRONMENT); AERODYNAMICS; info:eu-repo/classification/ddc/530; info:eu-repo/classification/ddc/710; Physics; Civic & landscape art

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Immer, M. C. (2016). Time-resolved measurement and simulation of local scale turbulent urban flow. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/112287

Chicago Manual of Style (16^th Edition):

Immer, Marc Christian. “Time-resolved measurement and simulation of local scale turbulent urban flow.” 2016. Doctoral Dissertation, ETH Zürich. Accessed February 28, 2021. http://hdl.handle.net/20.500.11850/112287.

MLA Handbook (7^th Edition):

Immer, Marc Christian. “Time-resolved measurement and simulation of local scale turbulent urban flow.” 2016. Web. 28 Feb 2021.

Vancouver:

Immer MC. Time-resolved measurement and simulation of local scale turbulent urban flow. [Internet] [Doctoral dissertation]. ETH Zürich; 2016. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/20.500.11850/112287.

Council of Science Editors:

Immer MC. Time-resolved measurement and simulation of local scale turbulent urban flow. [Doctoral Dissertation]. ETH Zürich; 2016. Available from: http://hdl.handle.net/20.500.11850/112287

22. Bergman, David. Modelling & implementation of Aerodynamic Zero-lift Drag into ADAPDT.

Degree: Design and Engineering, 2009, Mälardalen University

URL: http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-7459

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The objective of this thesis work was to construct and implement an algorithm into the programADAPDT to calculate the zero-lift drag profile for defined… (more)

▼

The objective of this thesis work was to construct and implement an algorithm into the programADAPDT to calculate the zero-lift drag profile for defined aircraft geometries. ADAPDT, shortfor AeroDynamic Analysis and Preliminary Design Tool, is a program that calculates forces andmoments about a flat plate geometry based on potential flow theory. Zero-lift drag will becalculated by means of different hand-book methods found suitable for the objective andapplicable to the geometry definition that ADAPDT utilizes. Drag has two main sources of origin: friction and pressure distribution, all drag acting on theaircraft can be traced back to one of these two physical phenomena. In aviation drag is dividedinto induced drag that depends on the lift produced and zero-lift drag that depends on the geometry of the aircraft. How reliable and accurate the zero-lift drag computations are depends on the geometry data thatcan be extracted and used. ADAPDT‟s geometry definition is limited to flat plate geometrieshowever although simple it has the potential to provide a huge amount of data and also delivergood results for the intended use. The flat plate representation of the geometry proved to beleast sufficient for the body while wing elements could be described with much more accuracy. Different empirical hand-book methods were used to create the zero-lift drag algorithm. Whenchoosing equations and formulas, great care had to be taken as to what input was required sothat ADAPDT could provide the corresponding output. At the same time the equations shouldnot be so basic that level of accuracy would be compromised beyond what should be expectedfrom the intended use. Finally, four well known aircraft configurations, with available zero-lift drag data, weremodeled with ADAPDT‟s flat plate geometry in order to validate, verify and evaluate the zeroliftdrag algorithm‟s magnitude of reliability. The results for conventional aircraft geometriesprovided a relative error within 0-15 % of the reference data given in the speed range of zero toMach 1.2. While for an aircraft with more complicated body geometry the error could go up to40 % in the same speed regime. But even though the limited geometry is grounds foruncertainties the final product provides ADAPDT with very good zero-lift drag estimationcapability earlier not available. A capability that overtime as ADAPDT continues to evolve hasthe potential to further develop in terms of improved accuracy.

Målet med detta examensarbete var att skapa och implementera en algoritm som införmöjligheten att beräkna nollmotstånd för givna flygplansgeometrier i programmet ADAPDT.ADAPDT, kort för AeroDynamic Analysis and Preliminary Design Tool, är ett program som,baserat på potential strömnings teori, beräknar krafter och moment på en geometri uppbyggd avplana plattor. Nollmotståndet kommer att baseras en kombination av handboksmetoder somfunnits lämpliga och applicerbara på geometridefinitionen given i ADAPDT. Motstånd har sitt ursprung i två fysikaliska…

Subjects/Keywords: drag; zero-lift drag; aerodynamics; nollmotsånd; aerodynamik; motstånd; Fluid mechanics; Strömningsmekanik; Vehicle engineering; Farkostteknik

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APA (6^th Edition):

Bergman, D. (2009). Modelling & implementation of Aerodynamic Zero-lift Drag into ADAPDT. (Thesis). Mälardalen University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-7459

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Bergman, David. “Modelling & implementation of Aerodynamic Zero-lift Drag into ADAPDT.” 2009. Thesis, Mälardalen University. Accessed February 28, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-7459.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Bergman, David. “Modelling & implementation of Aerodynamic Zero-lift Drag into ADAPDT.” 2009. Web. 28 Feb 2021.

Vancouver:

Bergman D. Modelling & implementation of Aerodynamic Zero-lift Drag into ADAPDT. [Internet] [Thesis]. Mälardalen University; 2009. [cited 2021 Feb 28]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-7459.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Bergman D. Modelling & implementation of Aerodynamic Zero-lift Drag into ADAPDT. [Thesis]. Mälardalen University; 2009. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-7459

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

23. Eriksson, Rasmus. Discars flygegenskaper : Baserat på aerodynamiska mätningar.

Degree: Quality Management and Mechanical Engineering, 2018, Mid Sweden University

URL: http://urn.kb.se/resolve?urn=urn:nbn:se:miun:diva-34794

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Detta projekt undersöker möjligheterna att bedöma discar avsedda för discgolf efter en skala grundad i vetenskapliga tester. Tester görs i vindtunneln hos… (more)

Subjects/Keywords: Discgolf; aerodynamics; flight ratings; Discgolf; aerodynamik; flygegenskaper; Other Mechanical Engineering; Annan maskinteknik

11 more images…

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APA (6^th Edition):

Eriksson, R. (2018). Discars flygegenskaper : Baserat på aerodynamiska mätningar. (Thesis). Mid Sweden University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:miun:diva-34794

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Eriksson, Rasmus. “Discars flygegenskaper : Baserat på aerodynamiska mätningar.” 2018. Thesis, Mid Sweden University. Accessed February 28, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:miun:diva-34794.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Eriksson, Rasmus. “Discars flygegenskaper : Baserat på aerodynamiska mätningar.” 2018. Web. 28 Feb 2021.

Vancouver:

Eriksson R. Discars flygegenskaper : Baserat på aerodynamiska mätningar. [Internet] [Thesis]. Mid Sweden University; 2018. [cited 2021 Feb 28]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:miun:diva-34794.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Eriksson R. Discars flygegenskaper : Baserat på aerodynamiska mätningar. [Thesis]. Mid Sweden University; 2018. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:miun:diva-34794

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

ETH Zürich

24. Gerber, Alfred. Untersuchungen über Grenzschichtabsaugung.

Degree: 1938, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/133090

Subjects/Keywords: GRENZSCHICHTABSAUGUNG + GRENZSCHICHTAUSBLASUNG (AERODYNAMIK); GRENZSCHICHTABLÖSUNG (FLUIDDYNAMIK); BOUNDARY LAYER SUCTION + BOUNDARY LAYER BLOWING (AERODYNAMICS); STALL (FLUID DYNAMICS); info:eu-repo/classification/ddc/530; Physics

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Gerber, A. (1938). Untersuchungen über Grenzschichtabsaugung. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/133090

Chicago Manual of Style (16^th Edition):

Gerber, Alfred. “Untersuchungen über Grenzschichtabsaugung.” 1938. Doctoral Dissertation, ETH Zürich. Accessed February 28, 2021. http://hdl.handle.net/20.500.11850/133090.

MLA Handbook (7^th Edition):

Gerber, Alfred. “Untersuchungen über Grenzschichtabsaugung.” 1938. Web. 28 Feb 2021.

Vancouver:

Gerber A. Untersuchungen über Grenzschichtabsaugung. [Internet] [Doctoral dissertation]. ETH Zürich; 1938. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/20.500.11850/133090.

Council of Science Editors:

Gerber A. Untersuchungen über Grenzschichtabsaugung. [Doctoral Dissertation]. ETH Zürich; 1938. Available from: http://hdl.handle.net/20.500.11850/133090

ETH Zürich

25. Houbolt, John Cornelius. A Study of several aerothermoelastic problems of aircraft structures in high-speed flight.

Degree: 1958, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/134942

Subjects/Keywords: AERODYNAMIK; WÄRMELEHRE; AERODYNAMICS; THERMOPHYSICS; info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/530; Engineering & allied operations; Physics

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APA (6^th Edition):

Houbolt, J. C. (1958). A Study of several aerothermoelastic problems of aircraft structures in high-speed flight. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/134942

Chicago Manual of Style (16^th Edition):

Houbolt, John Cornelius. “A Study of several aerothermoelastic problems of aircraft structures in high-speed flight.” 1958. Doctoral Dissertation, ETH Zürich. Accessed February 28, 2021. http://hdl.handle.net/20.500.11850/134942.

MLA Handbook (7^th Edition):

Houbolt, John Cornelius. “A Study of several aerothermoelastic problems of aircraft structures in high-speed flight.” 1958. Web. 28 Feb 2021.

Vancouver:

Houbolt JC. A Study of several aerothermoelastic problems of aircraft structures in high-speed flight. [Internet] [Doctoral dissertation]. ETH Zürich; 1958. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/20.500.11850/134942.

Council of Science Editors:

Houbolt JC. A Study of several aerothermoelastic problems of aircraft structures in high-speed flight. [Doctoral Dissertation]. ETH Zürich; 1958. Available from: http://hdl.handle.net/20.500.11850/134942

ETH Zürich

26. Meyer, Richard. Beitrag zur Theorie feststehender Schaufelgitter.

Degree: 1946, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/135220

Subjects/Keywords: SCHAUFELN (INNERE AERODYNAMIK); SCOOPS, BLADES (INTERNAL AERODYNAMICS); info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/530; Engineering & allied operations; Physics

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APA (6^th Edition):

Meyer, R. (1946). Beitrag zur Theorie feststehender Schaufelgitter. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/135220

Chicago Manual of Style (16^th Edition):

Meyer, Richard. “Beitrag zur Theorie feststehender Schaufelgitter.” 1946. Doctoral Dissertation, ETH Zürich. Accessed February 28, 2021. http://hdl.handle.net/20.500.11850/135220.

MLA Handbook (7^th Edition):

Meyer, Richard. “Beitrag zur Theorie feststehender Schaufelgitter.” 1946. Web. 28 Feb 2021.

Vancouver:

Meyer R. Beitrag zur Theorie feststehender Schaufelgitter. [Internet] [Doctoral dissertation]. ETH Zürich; 1946. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/20.500.11850/135220.

Council of Science Editors:

Meyer R. Beitrag zur Theorie feststehender Schaufelgitter. [Doctoral Dissertation]. ETH Zürich; 1946. Available from: http://hdl.handle.net/20.500.11850/135220

ETH Zürich

27. Ginsburg, Theo. Untersuchungen über die dreidimensionale Potentialströmung durch axiale Schaufelgitter.

Degree: 1956, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/137487

Subjects/Keywords: SCHAUFELN (INNERE AERODYNAMIK); POTENTIALSTRÖMUNG (FLUIDDYNAMIK); SCOOPS, BLADES (INTERNAL AERODYNAMICS); POTENTIAL FLOW (FLUID DYNAMICS); info:eu-repo/classification/ddc/530; Physics

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Ginsburg, T. (1956). Untersuchungen über die dreidimensionale Potentialströmung durch axiale Schaufelgitter. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/137487

Chicago Manual of Style (16^th Edition):

Ginsburg, Theo. “Untersuchungen über die dreidimensionale Potentialströmung durch axiale Schaufelgitter.” 1956. Doctoral Dissertation, ETH Zürich. Accessed February 28, 2021. http://hdl.handle.net/20.500.11850/137487.

MLA Handbook (7^th Edition):

Ginsburg, Theo. “Untersuchungen über die dreidimensionale Potentialströmung durch axiale Schaufelgitter.” 1956. Web. 28 Feb 2021.

Vancouver:

Ginsburg T. Untersuchungen über die dreidimensionale Potentialströmung durch axiale Schaufelgitter. [Internet] [Doctoral dissertation]. ETH Zürich; 1956. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/20.500.11850/137487.

Council of Science Editors:

Ginsburg T. Untersuchungen über die dreidimensionale Potentialströmung durch axiale Schaufelgitter. [Doctoral Dissertation]. ETH Zürich; 1956. Available from: http://hdl.handle.net/20.500.11850/137487

ETH Zürich

28. Sawyer, William Thomas. Experimental investigation of a stationary cascade of aerodynamic profiles.

Degree: 1949, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/146703

Subjects/Keywords: TURBOMASCHINENSCHAUFELN (TURBOMASCHINEN); AERODYNAMIK; TURBOMACHINE BLADES (TURBOMACHINES); AERODYNAMICS; info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/530; Engineering & allied operations; Physics

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Sawyer, W. T. (1949). Experimental investigation of a stationary cascade of aerodynamic profiles. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/146703

Chicago Manual of Style (16^th Edition):

Sawyer, William Thomas. “Experimental investigation of a stationary cascade of aerodynamic profiles.” 1949. Doctoral Dissertation, ETH Zürich. Accessed February 28, 2021. http://hdl.handle.net/20.500.11850/146703.

MLA Handbook (7^th Edition):

Sawyer, William Thomas. “Experimental investigation of a stationary cascade of aerodynamic profiles.” 1949. Web. 28 Feb 2021.

Vancouver:

Sawyer WT. Experimental investigation of a stationary cascade of aerodynamic profiles. [Internet] [Doctoral dissertation]. ETH Zürich; 1949. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/20.500.11850/146703.

Council of Science Editors:

Sawyer WT. Experimental investigation of a stationary cascade of aerodynamic profiles. [Doctoral Dissertation]. ETH Zürich; 1949. Available from: http://hdl.handle.net/20.500.11850/146703

ETH Zürich

29. Flomenhoft, Hubert Ivan. Investigation of effects of extreme structural flexibility on flight vehicles with feedback-control-system stabilization.

Degree: 1965, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/131737

Subjects/Keywords: AEROELASTIZITÄT (AERODYNAMIK); AEROELASTICITY (AERODYNAMICS); info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/530; Engineering & allied operations; Physics

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APA (6^th Edition):

Flomenhoft, H. I. (1965). Investigation of effects of extreme structural flexibility on flight vehicles with feedback-control-system stabilization. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/131737

Chicago Manual of Style (16^th Edition):

Flomenhoft, Hubert Ivan. “Investigation of effects of extreme structural flexibility on flight vehicles with feedback-control-system stabilization.” 1965. Doctoral Dissertation, ETH Zürich. Accessed February 28, 2021. http://hdl.handle.net/20.500.11850/131737.

MLA Handbook (7^th Edition):

Flomenhoft, Hubert Ivan. “Investigation of effects of extreme structural flexibility on flight vehicles with feedback-control-system stabilization.” 1965. Web. 28 Feb 2021.

Vancouver:

Flomenhoft HI. Investigation of effects of extreme structural flexibility on flight vehicles with feedback-control-system stabilization. [Internet] [Doctoral dissertation]. ETH Zürich; 1965. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/20.500.11850/131737.

Council of Science Editors:

Flomenhoft HI. Investigation of effects of extreme structural flexibility on flight vehicles with feedback-control-system stabilization. [Doctoral Dissertation]. ETH Zürich; 1965. Available from: http://hdl.handle.net/20.500.11850/131737

ETH Zürich

30. Mona, Alain G. Zur Bestimmung der Flügeleinflüsse auf die Rumpfnormalkräfte bei Flügel-Rumpf-Kombinationen im Ueberschall.

Degree: 1965, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/131853

Subjects/Keywords: INTERFERENZPROBLEME (AERODYNAMIK); INTERFERENCE PROBLEMS (AERODYNAMICS); info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/530; Engineering & allied operations; Physics

Record Details Similar Records Cite « Share

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APA (6^th Edition):

Mona, A. G. (1965). Zur Bestimmung der Flügeleinflüsse auf die Rumpfnormalkräfte bei Flügel-Rumpf-Kombinationen im Ueberschall. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/131853

Chicago Manual of Style (16^th Edition):

Mona, Alain G. “Zur Bestimmung der Flügeleinflüsse auf die Rumpfnormalkräfte bei Flügel-Rumpf-Kombinationen im Ueberschall.” 1965. Doctoral Dissertation, ETH Zürich. Accessed February 28, 2021. http://hdl.handle.net/20.500.11850/131853.

MLA Handbook (7^th Edition):

Mona, Alain G. “Zur Bestimmung der Flügeleinflüsse auf die Rumpfnormalkräfte bei Flügel-Rumpf-Kombinationen im Ueberschall.” 1965. Web. 28 Feb 2021.

Vancouver:

Mona AG. Zur Bestimmung der Flügeleinflüsse auf die Rumpfnormalkräfte bei Flügel-Rumpf-Kombinationen im Ueberschall. [Internet] [Doctoral dissertation]. ETH Zürich; 1965. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/20.500.11850/131853.

Council of Science Editors:

Mona AG. Zur Bestimmung der Flügeleinflüsse auf die Rumpfnormalkräfte bei Flügel-Rumpf-Kombinationen im Ueberschall. [Doctoral Dissertation]. ETH Zürich; 1965. Available from: http://hdl.handle.net/20.500.11850/131853

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