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You searched for subject:(drag polar). Showing records 1 – 16 of 16 total matches.

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Brno University of Technology

1. Kerndl, Jindřich. Analýza letových výkonů letounu VUT 081 KONDOR: Flight performance analysis of the airplane VUT 081 KONDOR.

Degree: 2019, Brno University of Technology

 The aim of this diploma thesis is to analyse flight performance of airplane VUT-081 Kondor. The first part focuses on determination and estimation of aerodynamic… (more)

Subjects/Keywords: polára letounu; výkonové charakteristiky motoru; letové výkony; CS-ELSA; drag polar; flight performance; engine performance data; CS-ELSA

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APA (6th Edition):

Kerndl, J. (2019). Analýza letových výkonů letounu VUT 081 KONDOR: Flight performance analysis of the airplane VUT 081 KONDOR. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/26897

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

Chicago Manual of Style (16th Edition):

Kerndl, Jindřich. “Analýza letových výkonů letounu VUT 081 KONDOR: Flight performance analysis of the airplane VUT 081 KONDOR.” 2019. Thesis, Brno University of Technology. Accessed January 26, 2021. http://hdl.handle.net/11012/26897.

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

MLA Handbook (7th Edition):

Kerndl, Jindřich. “Analýza letových výkonů letounu VUT 081 KONDOR: Flight performance analysis of the airplane VUT 081 KONDOR.” 2019. Web. 26 Jan 2021.

Vancouver:

Kerndl J. Analýza letových výkonů letounu VUT 081 KONDOR: Flight performance analysis of the airplane VUT 081 KONDOR. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 26]. Available from: http://hdl.handle.net/11012/26897.

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

Council of Science Editors:

Kerndl J. Analýza letových výkonů letounu VUT 081 KONDOR: Flight performance analysis of the airplane VUT 081 KONDOR. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/26897

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


Brno University of Technology

2. Foltýn, Pavel. Aerodynamické vlastnosti leteckých profilů: Aerodynamic characteristics of airfoils.

Degree: 2019, Brno University of Technology

 This bachelor´s thesis describes an influence of geometric characteristics of an airfoil on its aerodynamic properties. The first part of the thesis defines airfoil, describes… (more)

Subjects/Keywords: profil; geometrické charakteristiky; vztlaková čára; odporová čára; momentová čára; polára; aerodynamický tunel; airfoil; geometric characteristics; buoyancy line; drag line; moment line; polar; wind tunnel

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APA (6th Edition):

Foltýn, P. (2019). Aerodynamické vlastnosti leteckých profilů: Aerodynamic characteristics of airfoils. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/27703

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

Chicago Manual of Style (16th Edition):

Foltýn, Pavel. “Aerodynamické vlastnosti leteckých profilů: Aerodynamic characteristics of airfoils.” 2019. Thesis, Brno University of Technology. Accessed January 26, 2021. http://hdl.handle.net/11012/27703.

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

MLA Handbook (7th Edition):

Foltýn, Pavel. “Aerodynamické vlastnosti leteckých profilů: Aerodynamic characteristics of airfoils.” 2019. Web. 26 Jan 2021.

Vancouver:

Foltýn P. Aerodynamické vlastnosti leteckých profilů: Aerodynamic characteristics of airfoils. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 26]. Available from: http://hdl.handle.net/11012/27703.

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

Council of Science Editors:

Foltýn P. Aerodynamické vlastnosti leteckých profilů: Aerodynamic characteristics of airfoils. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/27703

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


Brno University of Technology

3. Podhorský, Matěj. Návrh základní koncepce air - mobilu: Conceptual design of air- mobil.

Degree: 2019, Brno University of Technology

 The topic of the thesis is a conceptual design of a roadable aircraft. The comparison of existing concepts is made, as well as description of… (more)

Subjects/Keywords: Air-mobil; koncepční návrh; létající automobil; obálka zatížení; polára; předpisová báze; příhradová konstrukce.; Air-mobile; aircraft concept design; roadable aircraft; flight and gust envelope; drag polar; certification specification; truss construction.

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APA (6th Edition):

Podhorský, M. (2019). Návrh základní koncepce air - mobilu: Conceptual design of air- mobil. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/33648

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

Chicago Manual of Style (16th Edition):

Podhorský, Matěj. “Návrh základní koncepce air - mobilu: Conceptual design of air- mobil.” 2019. Thesis, Brno University of Technology. Accessed January 26, 2021. http://hdl.handle.net/11012/33648.

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

MLA Handbook (7th Edition):

Podhorský, Matěj. “Návrh základní koncepce air - mobilu: Conceptual design of air- mobil.” 2019. Web. 26 Jan 2021.

Vancouver:

Podhorský M. Návrh základní koncepce air - mobilu: Conceptual design of air- mobil. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 26]. Available from: http://hdl.handle.net/11012/33648.

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

Council of Science Editors:

Podhorský M. Návrh základní koncepce air - mobilu: Conceptual design of air- mobil. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/33648

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


Brno University of Technology

4. Kóňa, Marián. Aerodynamický návrh transsonického bezpilotního kluzáku: Aerodynamic design of transonic UAV glider.

Degree: 2019, Brno University of Technology

 This master thesis is focused on aerodynamic design of transonic glider, which is assigned for following an airliner at cruising regime of flight. Main goal… (more)

Subjects/Keywords: Transsonika; kluzák; Whitcombovo pravidlo ploch; polára; hmotnostní rozbor; podélná statická stabilita; centráž; Transonic; glider; Whitcomb area rule; drag polar; mass analysis; longitudinal static stability; center of gravity position

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APA (6th Edition):

Kóňa, M. (2019). Aerodynamický návrh transsonického bezpilotního kluzáku: Aerodynamic design of transonic UAV glider. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/40280

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

Chicago Manual of Style (16th Edition):

Kóňa, Marián. “Aerodynamický návrh transsonického bezpilotního kluzáku: Aerodynamic design of transonic UAV glider.” 2019. Thesis, Brno University of Technology. Accessed January 26, 2021. http://hdl.handle.net/11012/40280.

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

MLA Handbook (7th Edition):

Kóňa, Marián. “Aerodynamický návrh transsonického bezpilotního kluzáku: Aerodynamic design of transonic UAV glider.” 2019. Web. 26 Jan 2021.

Vancouver:

Kóňa M. Aerodynamický návrh transsonického bezpilotního kluzáku: Aerodynamic design of transonic UAV glider. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 26]. Available from: http://hdl.handle.net/11012/40280.

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

Council of Science Editors:

Kóňa M. Aerodynamický návrh transsonického bezpilotního kluzáku: Aerodynamic design of transonic UAV glider. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/40280

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


Brno University of Technology

5. Smýkal, Michal. Koncepční studie lehkého dvoumotorového proudového letounu: Conceptual study of very light twin jet aircraft.

Degree: 2018, Brno University of Technology

 The topic of the thesis is a conceptual study of very light twin jet aircraft. The comparison of present aircrafts is made, as well as… (more)

Subjects/Keywords: Koncepční návrh; odporová polára; výkony letounu; obálka zatížení; náklady na vývoj; Aircraft concept design; drag polar; performance of the aircraft; flight and gust envelope; development costs.

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APA (6th Edition):

Smýkal, M. (2018). Koncepční studie lehkého dvoumotorového proudového letounu: Conceptual study of very light twin jet aircraft. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/39498

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

Chicago Manual of Style (16th Edition):

Smýkal, Michal. “Koncepční studie lehkého dvoumotorového proudového letounu: Conceptual study of very light twin jet aircraft.” 2018. Thesis, Brno University of Technology. Accessed January 26, 2021. http://hdl.handle.net/11012/39498.

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

MLA Handbook (7th Edition):

Smýkal, Michal. “Koncepční studie lehkého dvoumotorového proudového letounu: Conceptual study of very light twin jet aircraft.” 2018. Web. 26 Jan 2021.

Vancouver:

Smýkal M. Koncepční studie lehkého dvoumotorového proudového letounu: Conceptual study of very light twin jet aircraft. [Internet] [Thesis]. Brno University of Technology; 2018. [cited 2021 Jan 26]. Available from: http://hdl.handle.net/11012/39498.

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

Council of Science Editors:

Smýkal M. Koncepční studie lehkého dvoumotorového proudového letounu: Conceptual study of very light twin jet aircraft. [Thesis]. Brno University of Technology; 2018. Available from: http://hdl.handle.net/11012/39498

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


Brno University of Technology

6. Machala, Martin. Návrh dvoumístného kovového letounu s ohledem na nízkou cenu a jednoduchost stavby: Design of the two seater ultralight aircraft with consideration the price and simplicity of the construction.

Degree: 2015, Brno University of Technology

 The object of the diploma thesis is a conceptual layout of two-seater metal ultralight aircraft which has simple construction and with respect to low price.… (more)

Subjects/Keywords: Letoun; křídlo; UL-2; koncepce; technologičnost; odporová polára; aerodynamické charakteristiky; letové výkony.; Aircraft; wing; UL-2; design; technology; drag polar; aerodynamic characteristics; performance.

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APA (6th Edition):

Machala, M. (2015). Návrh dvoumístného kovového letounu s ohledem na nízkou cenu a jednoduchost stavby: Design of the two seater ultralight aircraft with consideration the price and simplicity of the construction. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/11251

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

Chicago Manual of Style (16th Edition):

Machala, Martin. “Návrh dvoumístného kovového letounu s ohledem na nízkou cenu a jednoduchost stavby: Design of the two seater ultralight aircraft with consideration the price and simplicity of the construction.” 2015. Thesis, Brno University of Technology. Accessed January 26, 2021. http://hdl.handle.net/11012/11251.

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

MLA Handbook (7th Edition):

Machala, Martin. “Návrh dvoumístného kovového letounu s ohledem na nízkou cenu a jednoduchost stavby: Design of the two seater ultralight aircraft with consideration the price and simplicity of the construction.” 2015. Web. 26 Jan 2021.

Vancouver:

Machala M. Návrh dvoumístného kovového letounu s ohledem na nízkou cenu a jednoduchost stavby: Design of the two seater ultralight aircraft with consideration the price and simplicity of the construction. [Internet] [Thesis]. Brno University of Technology; 2015. [cited 2021 Jan 26]. Available from: http://hdl.handle.net/11012/11251.

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

Council of Science Editors:

Machala M. Návrh dvoumístného kovového letounu s ohledem na nízkou cenu a jednoduchost stavby: Design of the two seater ultralight aircraft with consideration the price and simplicity of the construction. [Thesis]. Brno University of Technology; 2015. Available from: http://hdl.handle.net/11012/11251

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

7. Chase, Adam Thomas. Flight Testing Small UAVs for Aerodynamic Parameter Estimation.

Degree: MS, Aerospace Engineering, 2014, Cal Poly

  A flight data acquisition system was developed to aid unmanned vehicle designers in verifying the vehicle's design performance. The system is reconfigurable and allows… (more)

Subjects/Keywords: UAV; performance; design; testing; drag polar; system identification; Aeronautical Vehicles

…27 7.1 Clean Drag Polar Repeatability Testing : 𝐶 𝐷0 Regression Coefficient… …47 7.2 Clean Drag Polar Repeatability Testing : 𝐶1 Regression Coefficient . . . . . 47… …7.3 Clean Drag Polar Repeatability Testing : 𝐶2 Regression Coefficient . . . . . 47 7.4… …Slope with 𝐶1 From Flight and XFOIL . . . . . . . . . . . . . . . 52 7.7 Dirty Drag Polar… …Repeatability Testing : 𝐶 𝐷0 Regression Coefficient . . . . . 55 7.8 Dirty Drag Polar… 

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APA (6th Edition):

Chase, A. T. (2014). Flight Testing Small UAVs for Aerodynamic Parameter Estimation. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1191 ; 10.15368/theses.2014.38

Chicago Manual of Style (16th Edition):

Chase, Adam Thomas. “Flight Testing Small UAVs for Aerodynamic Parameter Estimation.” 2014. Masters Thesis, Cal Poly. Accessed January 26, 2021. https://digitalcommons.calpoly.edu/theses/1191 ; 10.15368/theses.2014.38.

MLA Handbook (7th Edition):

Chase, Adam Thomas. “Flight Testing Small UAVs for Aerodynamic Parameter Estimation.” 2014. Web. 26 Jan 2021.

Vancouver:

Chase AT. Flight Testing Small UAVs for Aerodynamic Parameter Estimation. [Internet] [Masters thesis]. Cal Poly; 2014. [cited 2021 Jan 26]. Available from: https://digitalcommons.calpoly.edu/theses/1191 ; 10.15368/theses.2014.38.

Council of Science Editors:

Chase AT. Flight Testing Small UAVs for Aerodynamic Parameter Estimation. [Masters Thesis]. Cal Poly; 2014. Available from: https://digitalcommons.calpoly.edu/theses/1191 ; 10.15368/theses.2014.38


Brigham Young University

8. Luke, Mark Elden. Predicting Drag Polars For Micro Air Vehicles.

Degree: MS, 2003, Brigham Young University

Drag polars for three Micro Air Vehicles (MAVs) were measured at Reynolds numbers of 70,000, 50,000, 30,000, and 10,000 and compared to predictions generated using… (more)

Subjects/Keywords: Micro Air Vehicle; MAV; low Reynolds number; drag polar; predicted vs. measured; wind tunnel; force balance; Cfe; equivalent skin friction coefficient; e0; oswald efficiency; CL; minD; lift coefficient; drag coefficient; drag polar prediction; angle of attack; wetted surface area ratio; wing loading; aspect ratio; parasite drag coefficient; drag due to lift; aerodynamics; Mechanical Engineering

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APA (6th Edition):

Luke, M. E. (2003). Predicting Drag Polars For Micro Air Vehicles. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1107&context=etd

Chicago Manual of Style (16th Edition):

Luke, Mark Elden. “Predicting Drag Polars For Micro Air Vehicles.” 2003. Masters Thesis, Brigham Young University. Accessed January 26, 2021. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1107&context=etd.

MLA Handbook (7th Edition):

Luke, Mark Elden. “Predicting Drag Polars For Micro Air Vehicles.” 2003. Web. 26 Jan 2021.

Vancouver:

Luke ME. Predicting Drag Polars For Micro Air Vehicles. [Internet] [Masters thesis]. Brigham Young University; 2003. [cited 2021 Jan 26]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1107&context=etd.

Council of Science Editors:

Luke ME. Predicting Drag Polars For Micro Air Vehicles. [Masters Thesis]. Brigham Young University; 2003. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1107&context=etd


Brigham Young University

9. Ostler, Jon N. Flight Testing Small, Electric Powered Unmanned Aerial Vehicles.

Degree: MS, 2006, Brigham Young University

 Flight testing methods are developed to find the drag polar for small UAVs powered by electric motors with fixed-pitch propellers. Wind tunnel testing was used… (more)

Subjects/Keywords: performance; flight test; flight testing; drag polar; UAV; small; electric powered; electric; unmanned; uninhabited; Mechanical Engineering

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APA (6th Edition):

Ostler, J. N. (2006). Flight Testing Small, Electric Powered Unmanned Aerial Vehicles. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1386&context=etd

Chicago Manual of Style (16th Edition):

Ostler, Jon N. “Flight Testing Small, Electric Powered Unmanned Aerial Vehicles.” 2006. Masters Thesis, Brigham Young University. Accessed January 26, 2021. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1386&context=etd.

MLA Handbook (7th Edition):

Ostler, Jon N. “Flight Testing Small, Electric Powered Unmanned Aerial Vehicles.” 2006. Web. 26 Jan 2021.

Vancouver:

Ostler JN. Flight Testing Small, Electric Powered Unmanned Aerial Vehicles. [Internet] [Masters thesis]. Brigham Young University; 2006. [cited 2021 Jan 26]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1386&context=etd.

Council of Science Editors:

Ostler JN. Flight Testing Small, Electric Powered Unmanned Aerial Vehicles. [Masters Thesis]. Brigham Young University; 2006. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1386&context=etd


Brno University of Technology

10. Bilčík, Adam. Porovnání možností panelových metod pro aerodynamickou analýzu profilů: Comparison of panel codes for aerodynamic analysis of airfoils.

Degree: 2019, Brno University of Technology

 The purpose of this study is to create an overview of currently the most used panel codes for computation of aerodynamic characteristics of 2D airfoils.… (more)

Subjects/Keywords: Panelová metóda; NACA 0012; profil krídla; XFOIL; JavaFoil; XFLR5; Aerodynamický tunel; súčiniteľ vztlaku; súčiniteľ odporu; koeficient klopivého momentu; aerodynamická polára; Panel Method; NACA 0012; Airfoil; XFOIL; JavaFoil; XFLR5; Wind tunnel; Lift coefficient; Drag coefficient; Pitching moment coefficient; Polar curve

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

APA (6th Edition):

Bilčík, A. (2019). Porovnání možností panelových metod pro aerodynamickou analýzu profilů: Comparison of panel codes for aerodynamic analysis of airfoils. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/33237

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

Chicago Manual of Style (16th Edition):

Bilčík, Adam. “Porovnání možností panelových metod pro aerodynamickou analýzu profilů: Comparison of panel codes for aerodynamic analysis of airfoils.” 2019. Thesis, Brno University of Technology. Accessed January 26, 2021. http://hdl.handle.net/11012/33237.

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

MLA Handbook (7th Edition):

Bilčík, Adam. “Porovnání možností panelových metod pro aerodynamickou analýzu profilů: Comparison of panel codes for aerodynamic analysis of airfoils.” 2019. Web. 26 Jan 2021.

Vancouver:

Bilčík A. Porovnání možností panelových metod pro aerodynamickou analýzu profilů: Comparison of panel codes for aerodynamic analysis of airfoils. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 26]. Available from: http://hdl.handle.net/11012/33237.

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

Council of Science Editors:

Bilčík A. Porovnání možností panelových metod pro aerodynamickou analýzu profilů: Comparison of panel codes for aerodynamic analysis of airfoils. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/33237

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


Brno University of Technology

11. Kozelský, Martin. Konstrukční návrh letounu Avia BH534 v ultralehkém provedení: Avia BH534 airplane design as ultralight.

Degree: 2018, Brno University of Technology

 The object of the diploma thesis is a preparation of fundamental bases for realization aerofoils of the replica of the biplane aircraft BH534 Avia. The… (more)

Subjects/Keywords: Základní rozměry; polára letounu; výkony letounu; manévrová a poryvová obálka; zatížení nosných ploch; konstrukce nosných ploch; pevnostní výpočet nosných ploch.; Basic dimensions; drag polar; performance of the aircraft; manoeuvre and gust envelope; aerofoils loading; aerofoils construction; aerofoils strenght calculation.

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

APA (6th Edition):

Kozelský, M. (2018). Konstrukční návrh letounu Avia BH534 v ultralehkém provedení: Avia BH534 airplane design as ultralight. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/1576

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

Chicago Manual of Style (16th Edition):

Kozelský, Martin. “Konstrukční návrh letounu Avia BH534 v ultralehkém provedení: Avia BH534 airplane design as ultralight.” 2018. Thesis, Brno University of Technology. Accessed January 26, 2021. http://hdl.handle.net/11012/1576.

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

MLA Handbook (7th Edition):

Kozelský, Martin. “Konstrukční návrh letounu Avia BH534 v ultralehkém provedení: Avia BH534 airplane design as ultralight.” 2018. Web. 26 Jan 2021.

Vancouver:

Kozelský M. Konstrukční návrh letounu Avia BH534 v ultralehkém provedení: Avia BH534 airplane design as ultralight. [Internet] [Thesis]. Brno University of Technology; 2018. [cited 2021 Jan 26]. Available from: http://hdl.handle.net/11012/1576.

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

Council of Science Editors:

Kozelský M. Konstrukční návrh letounu Avia BH534 v ultralehkém provedení: Avia BH534 airplane design as ultralight. [Thesis]. Brno University of Technology; 2018. Available from: http://hdl.handle.net/11012/1576

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


Brno University of Technology

12. Lipková, Alica. Návrh repliky letounu L-40 "Meta Sokol" - základní rozměry - technologie: Replica design of Aircraft "Meta Sokol" - Basic dimensions - technology.

Degree: 2018, Brno University of Technology

 The object of the diploma thesis is a preparation of fundamentals for realization for replica of the aircraft L-40 „Meta Sokol“ matching the requirements of… (more)

Subjects/Keywords: Geometrické parametry; odporová polára; momentová křivka; aerodynamický střed letounu; vrtulová charakteristika; letové výkony; hmotnostní obálka; technologičnost; Geometrical dimensions; drag polar; moment curve; aerodynamic centre of airplane; propeller characteristic; performance; weight envelope; technology

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

APA (6th Edition):

Lipková, A. (2018). Návrh repliky letounu L-40 "Meta Sokol" - základní rozměry - technologie: Replica design of Aircraft "Meta Sokol" - Basic dimensions - technology. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/1220

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

Chicago Manual of Style (16th Edition):

Lipková, Alica. “Návrh repliky letounu L-40 "Meta Sokol" - základní rozměry - technologie: Replica design of Aircraft "Meta Sokol" - Basic dimensions - technology.” 2018. Thesis, Brno University of Technology. Accessed January 26, 2021. http://hdl.handle.net/11012/1220.

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

MLA Handbook (7th Edition):

Lipková, Alica. “Návrh repliky letounu L-40 "Meta Sokol" - základní rozměry - technologie: Replica design of Aircraft "Meta Sokol" - Basic dimensions - technology.” 2018. Web. 26 Jan 2021.

Vancouver:

Lipková A. Návrh repliky letounu L-40 "Meta Sokol" - základní rozměry - technologie: Replica design of Aircraft "Meta Sokol" - Basic dimensions - technology. [Internet] [Thesis]. Brno University of Technology; 2018. [cited 2021 Jan 26]. Available from: http://hdl.handle.net/11012/1220.

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

Council of Science Editors:

Lipková A. Návrh repliky letounu L-40 "Meta Sokol" - základní rozměry - technologie: Replica design of Aircraft "Meta Sokol" - Basic dimensions - technology. [Thesis]. Brno University of Technology; 2018. Available from: http://hdl.handle.net/11012/1220

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

13. Hauber, Anna Miriam. Carrier momentum relaxation in highly doped polar semiconductors and semiconductor heterostructures.

Degree: 2016, University College Cork

 Highly doped polar semiconductors are essential components of today’s semiconductor industry. Most strikingly, transistors in modern electronic devices are polar semiconductor heterostructures. It is important… (more)

Subjects/Keywords: Polar semiconductors; Momentum relaxation; Carrier mobility; Plasmons; Polar optical phonons; Phonon drag; Landau damping; Two-dimensional semiconductors; Dielectric functions; Dynamic screening

…relaxation in doped polar semiconductors v Anna Miriam Hauber For Kitty and Thomas… …O’Regan to sending me his code to benchmark some of the calculations I did on polar… …relaxation in doped polar semiconductors vii Anna Miriam Hauber Acknowledgements I spent many… …in doped polar semiconductors viii Anna Miriam Hauber Abstract Abstract Highly doped… …polar semiconductors are essential components of today’s semiconductor industry. Most… 

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

APA (6th Edition):

Hauber, A. M. (2016). Carrier momentum relaxation in highly doped polar semiconductors and semiconductor heterostructures. (Thesis). University College Cork. Retrieved from http://hdl.handle.net/10468/3417

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

Chicago Manual of Style (16th Edition):

Hauber, Anna Miriam. “Carrier momentum relaxation in highly doped polar semiconductors and semiconductor heterostructures.” 2016. Thesis, University College Cork. Accessed January 26, 2021. http://hdl.handle.net/10468/3417.

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

MLA Handbook (7th Edition):

Hauber, Anna Miriam. “Carrier momentum relaxation in highly doped polar semiconductors and semiconductor heterostructures.” 2016. Web. 26 Jan 2021.

Vancouver:

Hauber AM. Carrier momentum relaxation in highly doped polar semiconductors and semiconductor heterostructures. [Internet] [Thesis]. University College Cork; 2016. [cited 2021 Jan 26]. Available from: http://hdl.handle.net/10468/3417.

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

Council of Science Editors:

Hauber AM. Carrier momentum relaxation in highly doped polar semiconductors and semiconductor heterostructures. [Thesis]. University College Cork; 2016. Available from: http://hdl.handle.net/10468/3417

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


Delft University of Technology

14. Sun, J. Open Aircraft Performance Modeling: Based on an Analysis of Aircraft Surveillance Data.

Degree: 2019, Delft University of Technology

 A large number of stakeholders exist in the modern air traffic management ecosystem. Air transportation studies benefit from collaboration and the sharing of knowledge and… (more)

Subjects/Keywords: Aircraft Performance; Air Traffic Management; ADS-B; Drag Polar; Dynamic Model; Engine Fuel Flow; Kinematic Model; Meteo-Particle; Mode-S; Open Data; State Estimation; Thrust

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

APA (6th Edition):

Sun, J. (2019). Open Aircraft Performance Modeling: Based on an Analysis of Aircraft Surveillance Data. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:af94d535-1853-4a6c-8b3f-77c98a52346a ; urn:NBN:nl:ui:24-uuid:af94d535-1853-4a6c-8b3f-77c98a52346a ; af94d535-1853-4a6c-8b3f-77c98a52346a ; 10.4233/uuid:af94d535-1853-4a6c-8b3f-77c98a52346a ; urn:isbn:978-94-6384-030-9 ; urn:NBN:nl:ui:24-uuid:af94d535-1853-4a6c-8b3f-77c98a52346a ; http://resolver.tudelft.nl/uuid:af94d535-1853-4a6c-8b3f-77c98a52346a

Chicago Manual of Style (16th Edition):

Sun, J. “Open Aircraft Performance Modeling: Based on an Analysis of Aircraft Surveillance Data.” 2019. Doctoral Dissertation, Delft University of Technology. Accessed January 26, 2021. http://resolver.tudelft.nl/uuid:af94d535-1853-4a6c-8b3f-77c98a52346a ; urn:NBN:nl:ui:24-uuid:af94d535-1853-4a6c-8b3f-77c98a52346a ; af94d535-1853-4a6c-8b3f-77c98a52346a ; 10.4233/uuid:af94d535-1853-4a6c-8b3f-77c98a52346a ; urn:isbn:978-94-6384-030-9 ; urn:NBN:nl:ui:24-uuid:af94d535-1853-4a6c-8b3f-77c98a52346a ; http://resolver.tudelft.nl/uuid:af94d535-1853-4a6c-8b3f-77c98a52346a.

MLA Handbook (7th Edition):

Sun, J. “Open Aircraft Performance Modeling: Based on an Analysis of Aircraft Surveillance Data.” 2019. Web. 26 Jan 2021.

Vancouver:

Sun J. Open Aircraft Performance Modeling: Based on an Analysis of Aircraft Surveillance Data. [Internet] [Doctoral dissertation]. Delft University of Technology; 2019. [cited 2021 Jan 26]. Available from: http://resolver.tudelft.nl/uuid:af94d535-1853-4a6c-8b3f-77c98a52346a ; urn:NBN:nl:ui:24-uuid:af94d535-1853-4a6c-8b3f-77c98a52346a ; af94d535-1853-4a6c-8b3f-77c98a52346a ; 10.4233/uuid:af94d535-1853-4a6c-8b3f-77c98a52346a ; urn:isbn:978-94-6384-030-9 ; urn:NBN:nl:ui:24-uuid:af94d535-1853-4a6c-8b3f-77c98a52346a ; http://resolver.tudelft.nl/uuid:af94d535-1853-4a6c-8b3f-77c98a52346a.

Council of Science Editors:

Sun J. Open Aircraft Performance Modeling: Based on an Analysis of Aircraft Surveillance Data. [Doctoral Dissertation]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:af94d535-1853-4a6c-8b3f-77c98a52346a ; urn:NBN:nl:ui:24-uuid:af94d535-1853-4a6c-8b3f-77c98a52346a ; af94d535-1853-4a6c-8b3f-77c98a52346a ; 10.4233/uuid:af94d535-1853-4a6c-8b3f-77c98a52346a ; urn:isbn:978-94-6384-030-9 ; urn:NBN:nl:ui:24-uuid:af94d535-1853-4a6c-8b3f-77c98a52346a ; http://resolver.tudelft.nl/uuid:af94d535-1853-4a6c-8b3f-77c98a52346a


North Carolina State University

15. McAvoy, Christopher William. Analytical and Experimental Approaches to Airfoil-Aircraft Design Integration.

Degree: MS, Aerospace Engineering, 2002, North Carolina State University

 The aerodynamic characteristics of the wing airfoil are critical to achieving desired aircraft performance. However, even with all of the advances in airfoil and aircraft… (more)

Subjects/Keywords: aircraft performance; airfoil; aircraft; design; newton method; optimization; laminar flow; cruise flap; automatic flap; camber; trailing-edge flap; subsonic; general aviation; thin airfoil theory; UAV; stagnation point; low speed flow; low reynolds number; wind tunnel; NLF; drag polar; drag bucket; XFOIL; low-drag range; design integration; aerospace engineering; aeronautical; airfoil model construction; pressure distributions; trim effects; trim considerations; surface pressure sensing

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

APA (6th Edition):

McAvoy, C. W. (2002). Analytical and Experimental Approaches to Airfoil-Aircraft Design Integration. (Thesis). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/7

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

Chicago Manual of Style (16th Edition):

McAvoy, Christopher William. “Analytical and Experimental Approaches to Airfoil-Aircraft Design Integration.” 2002. Thesis, North Carolina State University. Accessed January 26, 2021. http://www.lib.ncsu.edu/resolver/1840.16/7.

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

MLA Handbook (7th Edition):

McAvoy, Christopher William. “Analytical and Experimental Approaches to Airfoil-Aircraft Design Integration.” 2002. Web. 26 Jan 2021.

Vancouver:

McAvoy CW. Analytical and Experimental Approaches to Airfoil-Aircraft Design Integration. [Internet] [Thesis]. North Carolina State University; 2002. [cited 2021 Jan 26]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/7.

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

Council of Science Editors:

McAvoy CW. Analytical and Experimental Approaches to Airfoil-Aircraft Design Integration. [Thesis]. North Carolina State University; 2002. Available from: http://www.lib.ncsu.edu/resolver/1840.16/7

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

16. Rao, Arjun. Measurement of aerodynamic characteristics of MAVs using motion tracking.

Degree: MS, 4048, 2012, University of Illinois – Urbana-Champaign

 Aerodynamic characteristics of Micro Air Vehicles (MAVs) is not well addressed in aeronautics literature, and more experimental data are required to help better understand the… (more)

Subjects/Keywords: Micro air vehicle (MAV); Reynolds number; remote controlled (RC); aircraft; airplane; model; Lift; drag; thrust; moment; stability; control; pitch; roll; yaw; weathercock; weathervane; motion tracking; motion capture; VICON; camera; wand; Re; lift curve; drag polar; propeller; Advanced Precision Composites (APC); sport; E-flite; sideslip; static margin (SM); axis; axes; PropellerScanner; airfoil; wing; lifting line theory; theory; experimental; Aerodynamics; calibration; noise; markers; camera; Euler angles; longitudinal; lateral; advance ratio; density; data points; Extra 260; Extra 300 3D; glider; frequency; revolutions per minute (RPM); body-fixed; Earth-fixed; transformation; rotation; matrix; filter; low-pass; finite difference; robust; lineqar; least-squares; parabolic; Uhlig; Selig; Rao

…25 25 26 27 27 28 29 30 31 32 4.1 4.2 4.3 Experimentally determined drag polar and lift… …angle of attack for the Extra 300 3D Experimentally determined drag polar and lift curve of… …determined drag polar and lift curve for the Extra 300 3D in glide and powered flight… …Comparison of experimentally determined drag polar and lift curve for the Extra 300 3D in glide and… …Comparison of experimentally determined drag polar and lift curve for the Extra 300 3D in glide and… 

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

APA (6th Edition):

Rao, A. (2012). Measurement of aerodynamic characteristics of MAVs using motion tracking. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/30943

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

Chicago Manual of Style (16th Edition):

Rao, Arjun. “Measurement of aerodynamic characteristics of MAVs using motion tracking.” 2012. Thesis, University of Illinois – Urbana-Champaign. Accessed January 26, 2021. http://hdl.handle.net/2142/30943.

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

MLA Handbook (7th Edition):

Rao, Arjun. “Measurement of aerodynamic characteristics of MAVs using motion tracking.” 2012. Web. 26 Jan 2021.

Vancouver:

Rao A. Measurement of aerodynamic characteristics of MAVs using motion tracking. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2012. [cited 2021 Jan 26]. Available from: http://hdl.handle.net/2142/30943.

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

Council of Science Editors:

Rao A. Measurement of aerodynamic characteristics of MAVs using motion tracking. [Thesis]. University of Illinois – Urbana-Champaign; 2012. Available from: http://hdl.handle.net/2142/30943

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

.