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You searched for subject:(Process of in flight aircraft icing). Showing records 1 – 30 of 351062 total matches.

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1. Pena, Dorian. Développement d'un code de givrage tridimensionnel avec méthode Level-Set : Development of a three-dimensional icing code using level-set method.

Degree: Docteur es, Mécanique des fluides, 2016, Strasbourg; Ecole polytechnique (Montréal, Canada)

Le travail réalisé dans cette thèse introduit le concept de l'utilisation de la méthode Level-Set pour simuler l'interface Glace/Air au cours du temps lors du… (more)

Subjects/Keywords: Givrage; Méthode Eulérienne de transport de particules; Thermodynamique du givrage; Méthode Level-Set; Méthode chimère; Icing; Eulerian approach; Process of in-flight aircraft icing; Level-Set method; Chimeria method; Navier-Stokes-Multi-Blocks; 629.1; 532.5

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APA (6th Edition):

Pena, D. (2016). Développement d'un code de givrage tridimensionnel avec méthode Level-Set : Development of a three-dimensional icing code using level-set method. (Doctoral Dissertation). Strasbourg; Ecole polytechnique (Montréal, Canada). Retrieved from http://www.theses.fr/2016STRAD014

Chicago Manual of Style (16th Edition):

Pena, Dorian. “Développement d'un code de givrage tridimensionnel avec méthode Level-Set : Development of a three-dimensional icing code using level-set method.” 2016. Doctoral Dissertation, Strasbourg; Ecole polytechnique (Montréal, Canada). Accessed March 07, 2021. http://www.theses.fr/2016STRAD014.

MLA Handbook (7th Edition):

Pena, Dorian. “Développement d'un code de givrage tridimensionnel avec méthode Level-Set : Development of a three-dimensional icing code using level-set method.” 2016. Web. 07 Mar 2021.

Vancouver:

Pena D. Développement d'un code de givrage tridimensionnel avec méthode Level-Set : Development of a three-dimensional icing code using level-set method. [Internet] [Doctoral dissertation]. Strasbourg; Ecole polytechnique (Montréal, Canada); 2016. [cited 2021 Mar 07]. Available from: http://www.theses.fr/2016STRAD014.

Council of Science Editors:

Pena D. Développement d'un code de givrage tridimensionnel avec méthode Level-Set : Development of a three-dimensional icing code using level-set method. [Doctoral Dissertation]. Strasbourg; Ecole polytechnique (Montréal, Canada); 2016. Available from: http://www.theses.fr/2016STRAD014


Iowa State University

2. Li, Haixing. Experimental studies on the dynamics of in-flight and impacting water droplets pertinent to aircraft icing phenomena.

Degree: 2017, Iowa State University

Aircraft icing is widely recognized as a significant hazard to aircraft operations in cold weather. When an aircraft or rotorcraft fly in a cold climate,… (more)

Subjects/Keywords: 3-D shape reconstruction of impact droplet; Aircraft icing; Droplet impact dynamics; Droplet impact on super-hydrophobic surface; In-flight droplets temperature measurement; Aerospace Engineering

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APA (6th Edition):

Li, H. (2017). Experimental studies on the dynamics of in-flight and impacting water droplets pertinent to aircraft icing phenomena. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/15564

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):

Li, Haixing. “Experimental studies on the dynamics of in-flight and impacting water droplets pertinent to aircraft icing phenomena.” 2017. Thesis, Iowa State University. Accessed March 07, 2021. https://lib.dr.iastate.edu/etd/15564.

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

MLA Handbook (7th Edition):

Li, Haixing. “Experimental studies on the dynamics of in-flight and impacting water droplets pertinent to aircraft icing phenomena.” 2017. Web. 07 Mar 2021.

Vancouver:

Li H. Experimental studies on the dynamics of in-flight and impacting water droplets pertinent to aircraft icing phenomena. [Internet] [Thesis]. Iowa State University; 2017. [cited 2021 Mar 07]. Available from: https://lib.dr.iastate.edu/etd/15564.

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

Council of Science Editors:

Li H. Experimental studies on the dynamics of in-flight and impacting water droplets pertinent to aircraft icing phenomena. [Thesis]. Iowa State University; 2017. Available from: https://lib.dr.iastate.edu/etd/15564

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


Brno University of Technology

3. Čížková, Markéta. Využití GPS pro měření za letu: Use GPS for in flight measurement.

Degree: 2019, Brno University of Technology

 Bachelor thesis Use GPS for In-Flight Measurement addresses the applicability of Global Positioning System as a tool for aircraft certification. The theoretical part of thesis… (more)

Subjects/Keywords: GPS; letadla; letové zkoušky; metody zkoušení letadel; zkoušení za letu; Aircraft; flight test; GPS; In-Flight Measurement; methods of aircraft testing

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APA (6th Edition):

Čížková, M. (2019). Využití GPS pro měření za letu: Use GPS for in flight measurement. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/176617

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):

Čížková, Markéta. “Využití GPS pro měření za letu: Use GPS for in flight measurement.” 2019. Thesis, Brno University of Technology. Accessed March 07, 2021. http://hdl.handle.net/11012/176617.

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

MLA Handbook (7th Edition):

Čížková, Markéta. “Využití GPS pro měření za letu: Use GPS for in flight measurement.” 2019. Web. 07 Mar 2021.

Vancouver:

Čížková M. Využití GPS pro měření za letu: Use GPS for in flight measurement. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/11012/176617.

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

Council of Science Editors:

Čížková M. Využití GPS pro měření za letu: Use GPS for in flight measurement. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/176617

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


Tampere University

4. Maly, Yahya. Cold Sprayed SLIPS Coatings: A pathway towards process optimization and icephobicity .

Degree: 2020, Tampere University

 Ice accretion is a major problem that causes economic loss, damages structure, impedes transports, and potentially leads to human injury and death. There is a… (more)

Subjects/Keywords: Icephobicity ; Aircraft icing ; Ice wind tunnel ; Anti-icing ; De-icing ; Passive anti-ice systems ; Icephobic coatings ; Sprayed coatings ; Hydrophobicity ; superhydrophobicity ; Nature-inspired technology ; Lotus Effect ; SLIPS ; Slippery Liquid Infused Porous Surfaces ; Thermal spraying technology ; Cold spraying of polymers ; Flame spraying ; Process development

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APA (6th Edition):

Maly, Y. (2020). Cold Sprayed SLIPS Coatings: A pathway towards process optimization and icephobicity . (Masters Thesis). Tampere University. Retrieved from https://trepo.tuni.fi/handle/10024/122358

Chicago Manual of Style (16th Edition):

Maly, Yahya. “Cold Sprayed SLIPS Coatings: A pathway towards process optimization and icephobicity .” 2020. Masters Thesis, Tampere University. Accessed March 07, 2021. https://trepo.tuni.fi/handle/10024/122358.

MLA Handbook (7th Edition):

Maly, Yahya. “Cold Sprayed SLIPS Coatings: A pathway towards process optimization and icephobicity .” 2020. Web. 07 Mar 2021.

Vancouver:

Maly Y. Cold Sprayed SLIPS Coatings: A pathway towards process optimization and icephobicity . [Internet] [Masters thesis]. Tampere University; 2020. [cited 2021 Mar 07]. Available from: https://trepo.tuni.fi/handle/10024/122358.

Council of Science Editors:

Maly Y. Cold Sprayed SLIPS Coatings: A pathway towards process optimization and icephobicity . [Masters Thesis]. Tampere University; 2020. Available from: https://trepo.tuni.fi/handle/10024/122358

5. Droz, Christophe. Guidage des ondes d'ordre élevé dans les composites : application au dégivrage en vol des pales d'hélicoptères : High-order wave propagation in composite waveguides : application to in-flight de-icing of helicopter rotor blades.

Degree: Docteur es, Dynamique des structures, 2015, Ecully, Ecole centrale de Lyon

Lorsqu’un hélicoptère opère dans des conditions givrantes extrêmes, l’accumulation de glace sur les pales peut considérablement impacter les performances de l’appareil. De nombreuses recherches portant… (more)

Subjects/Keywords: Pales d'hélicoptères; Dégivrage en vol; Helicopter rotor; In-flight de-icing

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APA (6th Edition):

Droz, C. (2015). Guidage des ondes d'ordre élevé dans les composites : application au dégivrage en vol des pales d'hélicoptères : High-order wave propagation in composite waveguides : application to in-flight de-icing of helicopter rotor blades. (Doctoral Dissertation). Ecully, Ecole centrale de Lyon. Retrieved from http://www.theses.fr/2015ECDL0026

Chicago Manual of Style (16th Edition):

Droz, Christophe. “Guidage des ondes d'ordre élevé dans les composites : application au dégivrage en vol des pales d'hélicoptères : High-order wave propagation in composite waveguides : application to in-flight de-icing of helicopter rotor blades.” 2015. Doctoral Dissertation, Ecully, Ecole centrale de Lyon. Accessed March 07, 2021. http://www.theses.fr/2015ECDL0026.

MLA Handbook (7th Edition):

Droz, Christophe. “Guidage des ondes d'ordre élevé dans les composites : application au dégivrage en vol des pales d'hélicoptères : High-order wave propagation in composite waveguides : application to in-flight de-icing of helicopter rotor blades.” 2015. Web. 07 Mar 2021.

Vancouver:

Droz C. Guidage des ondes d'ordre élevé dans les composites : application au dégivrage en vol des pales d'hélicoptères : High-order wave propagation in composite waveguides : application to in-flight de-icing of helicopter rotor blades. [Internet] [Doctoral dissertation]. Ecully, Ecole centrale de Lyon; 2015. [cited 2021 Mar 07]. Available from: http://www.theses.fr/2015ECDL0026.

Council of Science Editors:

Droz C. Guidage des ondes d'ordre élevé dans les composites : application au dégivrage en vol des pales d'hélicoptères : High-order wave propagation in composite waveguides : application to in-flight de-icing of helicopter rotor blades. [Doctoral Dissertation]. Ecully, Ecole centrale de Lyon; 2015. Available from: http://www.theses.fr/2015ECDL0026


University of Waterloo

6. Geiger, Paul. Simulation of In-Flight Rime Icing Using a Non-Body-Fitted Mesh.

Degree: 2020, University of Waterloo

 In-flight rime icing occurs when supercooled droplets strike the surface of an aircraft and instantly freeze. This often occurs in the high moisture, cold environments… (more)

Subjects/Keywords: in-flight icing; rime icing; immersed boundary method; cut-cell method; finite volume method; level set method; non-body-fitted mesh

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APA (6th Edition):

Geiger, P. (2020). Simulation of In-Flight Rime Icing Using a Non-Body-Fitted Mesh. (Thesis). University of Waterloo. Retrieved from http://hdl.handle.net/10012/15810

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):

Geiger, Paul. “Simulation of In-Flight Rime Icing Using a Non-Body-Fitted Mesh.” 2020. Thesis, University of Waterloo. Accessed March 07, 2021. http://hdl.handle.net/10012/15810.

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

MLA Handbook (7th Edition):

Geiger, Paul. “Simulation of In-Flight Rime Icing Using a Non-Body-Fitted Mesh.” 2020. Web. 07 Mar 2021.

Vancouver:

Geiger P. Simulation of In-Flight Rime Icing Using a Non-Body-Fitted Mesh. [Internet] [Thesis]. University of Waterloo; 2020. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/10012/15810.

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

Council of Science Editors:

Geiger P. Simulation of In-Flight Rime Icing Using a Non-Body-Fitted Mesh. [Thesis]. University of Waterloo; 2020. Available from: http://hdl.handle.net/10012/15810

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


Baylor University

7. Shannon, Timothy Andrew, 1991-. Convection from realistic ice roughness on a simulated NACA 0012 airfoil.

Degree: M.S.M.E., Baylor University. School of Engineering., 2015, Baylor University

 Ice roughness properties are critically important to the development of ice accretions on aircraft surfaces. Ice accretions degrade aircraft performance by increasing the skin friction… (more)

Subjects/Keywords: Aircraft icing. Ice roughness.

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APA (6th Edition):

Shannon, Timothy Andrew, 1. (2015). Convection from realistic ice roughness on a simulated NACA 0012 airfoil. (Masters Thesis). Baylor University. Retrieved from http://hdl.handle.net/2104/9534

Chicago Manual of Style (16th Edition):

Shannon, Timothy Andrew, 1991-. “Convection from realistic ice roughness on a simulated NACA 0012 airfoil.” 2015. Masters Thesis, Baylor University. Accessed March 07, 2021. http://hdl.handle.net/2104/9534.

MLA Handbook (7th Edition):

Shannon, Timothy Andrew, 1991-. “Convection from realistic ice roughness on a simulated NACA 0012 airfoil.” 2015. Web. 07 Mar 2021.

Vancouver:

Shannon, Timothy Andrew 1. Convection from realistic ice roughness on a simulated NACA 0012 airfoil. [Internet] [Masters thesis]. Baylor University; 2015. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/2104/9534.

Council of Science Editors:

Shannon, Timothy Andrew 1. Convection from realistic ice roughness on a simulated NACA 0012 airfoil. [Masters Thesis]. Baylor University; 2015. Available from: http://hdl.handle.net/2104/9534

8. Andersson, Daniel. The performance of an iced aircraft wing.

Degree: Engineering Science, 2011, University West

  The goal of this thesis work has been to develop and manufacture an ice layer which was to be mounted on the tip of… (more)

Subjects/Keywords: Airfoil; ice layer; in-flight icing; wind tunnel; rapid prototyping; lift force

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APA (6th Edition):

Andersson, D. (2011). The performance of an iced aircraft wing. (Thesis). University West. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:hv:diva-4098

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):

Andersson, Daniel. “The performance of an iced aircraft wing.” 2011. Thesis, University West. Accessed March 07, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:hv:diva-4098.

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

MLA Handbook (7th Edition):

Andersson, Daniel. “The performance of an iced aircraft wing.” 2011. Web. 07 Mar 2021.

Vancouver:

Andersson D. The performance of an iced aircraft wing. [Internet] [Thesis]. University West; 2011. [cited 2021 Mar 07]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:hv:diva-4098.

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

Council of Science Editors:

Andersson D. The performance of an iced aircraft wing. [Thesis]. University West; 2011. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:hv:diva-4098

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


Brno University of Technology

9. Fazekaš, Slavomír. Odmrazovací soustavy letadel: Aircraft de-icing systems.

Degree: 2018, Brno University of Technology

 The aim of my bachelor thesis is to make the acquaintance of the danger of ice coating on airplanes, it s creation and the way… (more)

Subjects/Keywords: Lietadlo; námraza; lietadlové systémy; protinámrazový systém; odmrazovanie; Aircraft; icing; aircraft systems; anti-icing; de-icing

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

APA (6th Edition):

Fazekaš, S. (2018). Odmrazovací soustavy letadel: Aircraft de-icing systems. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/27286

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):

Fazekaš, Slavomír. “Odmrazovací soustavy letadel: Aircraft de-icing systems.” 2018. Thesis, Brno University of Technology. Accessed March 07, 2021. http://hdl.handle.net/11012/27286.

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

MLA Handbook (7th Edition):

Fazekaš, Slavomír. “Odmrazovací soustavy letadel: Aircraft de-icing systems.” 2018. Web. 07 Mar 2021.

Vancouver:

Fazekaš S. Odmrazovací soustavy letadel: Aircraft de-icing systems. [Internet] [Thesis]. Brno University of Technology; 2018. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/11012/27286.

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

Council of Science Editors:

Fazekaš S. Odmrazovací soustavy letadel: Aircraft de-icing systems. [Thesis]. Brno University of Technology; 2018. Available from: http://hdl.handle.net/11012/27286

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


University of Ottawa

10. Nicklin, Sean. Hopping the Pond: The Normalization of North Atlantic Civil Aviation from its Origins to the Rise of the Jumbo Jet, 1919-1970 .

Degree: 2016, University of Ottawa

Flight across the North Atlantic is a routine process now, with thousands of flights carrying millions of passengers between Europe and North America every year… (more)

Subjects/Keywords: civil aviation; commercial flight; North Atlantic; transatlantic; aircraft; infrastructure; history of technology; history of flight

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APA (6th Edition):

Nicklin, S. (2016). Hopping the Pond: The Normalization of North Atlantic Civil Aviation from its Origins to the Rise of the Jumbo Jet, 1919-1970 . (Thesis). University of Ottawa. Retrieved from http://hdl.handle.net/10393/35298

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):

Nicklin, Sean. “Hopping the Pond: The Normalization of North Atlantic Civil Aviation from its Origins to the Rise of the Jumbo Jet, 1919-1970 .” 2016. Thesis, University of Ottawa. Accessed March 07, 2021. http://hdl.handle.net/10393/35298.

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

MLA Handbook (7th Edition):

Nicklin, Sean. “Hopping the Pond: The Normalization of North Atlantic Civil Aviation from its Origins to the Rise of the Jumbo Jet, 1919-1970 .” 2016. Web. 07 Mar 2021.

Vancouver:

Nicklin S. Hopping the Pond: The Normalization of North Atlantic Civil Aviation from its Origins to the Rise of the Jumbo Jet, 1919-1970 . [Internet] [Thesis]. University of Ottawa; 2016. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/10393/35298.

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

Council of Science Editors:

Nicklin S. Hopping the Pond: The Normalization of North Atlantic Civil Aviation from its Origins to the Rise of the Jumbo Jet, 1919-1970 . [Thesis]. University of Ottawa; 2016. Available from: http://hdl.handle.net/10393/35298

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


Penn State University

11. Soltis, Jared T. Design and Testing of an Erosion Resistant Ultrasonic De-icing System for Rotorcraft Blades.

Degree: 2013, Penn State University

 The goal of this research was to design a helicopter rotor blade lead edge that had high sand erosion resistance and was conducive to ultrasonic… (more)

Subjects/Keywords: aircraft icing; de-icing systems; ice adhesion strength; ultrasonic de-icing; erosion resistant materials

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APA (6th Edition):

Soltis, J. T. (2013). Design and Testing of an Erosion Resistant Ultrasonic De-icing System for Rotorcraft Blades. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/19062

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):

Soltis, Jared T. “Design and Testing of an Erosion Resistant Ultrasonic De-icing System for Rotorcraft Blades.” 2013. Thesis, Penn State University. Accessed March 07, 2021. https://submit-etda.libraries.psu.edu/catalog/19062.

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

MLA Handbook (7th Edition):

Soltis, Jared T. “Design and Testing of an Erosion Resistant Ultrasonic De-icing System for Rotorcraft Blades.” 2013. Web. 07 Mar 2021.

Vancouver:

Soltis JT. Design and Testing of an Erosion Resistant Ultrasonic De-icing System for Rotorcraft Blades. [Internet] [Thesis]. Penn State University; 2013. [cited 2021 Mar 07]. Available from: https://submit-etda.libraries.psu.edu/catalog/19062.

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

Council of Science Editors:

Soltis JT. Design and Testing of an Erosion Resistant Ultrasonic De-icing System for Rotorcraft Blades. [Thesis]. Penn State University; 2013. Available from: https://submit-etda.libraries.psu.edu/catalog/19062

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


Brno University of Technology

12. Smékal, Aleš. Odmrazovací soustavy letadel: Aircraft de-icing systems.

Degree: 2019, Brno University of Technology

 The bachelor´s thesis is familiarization of me with icing on aircrafts. It includes the distribution systems for anti-icing and de-icing, energy intensity and efficiency are… (more)

Subjects/Keywords: Námraza; protinámrazový; letadlové systémy; led; odmrazování; Icing; anti-icing; aircraft systems; ice; de-icing

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

APA (6th Edition):

Smékal, A. (2019). Odmrazovací soustavy letadel: Aircraft de-icing systems. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/33535

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):

Smékal, Aleš. “Odmrazovací soustavy letadel: Aircraft de-icing systems.” 2019. Thesis, Brno University of Technology. Accessed March 07, 2021. http://hdl.handle.net/11012/33535.

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

MLA Handbook (7th Edition):

Smékal, Aleš. “Odmrazovací soustavy letadel: Aircraft de-icing systems.” 2019. Web. 07 Mar 2021.

Vancouver:

Smékal A. Odmrazovací soustavy letadel: Aircraft de-icing systems. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/11012/33535.

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

Council of Science Editors:

Smékal A. Odmrazovací soustavy letadel: Aircraft de-icing systems. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/33535

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


University of Missouri – Kansas City

13. Alabsi, Mohammed. In-Flight Learning Based Flight Control of an Unmanned Aircraft System.

Degree: 2018, University of Missouri – Kansas City

 Unmanned Aerial Vehicles (UAVs) popularity has increased substantially in the last few years. UAVs capabilities continue to improve as a result of advances in battery… (more)

Subjects/Keywords: Drone aircraft; Flight control; Dissertation  – University of Missouri – Kansas City  – Engineering

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APA (6th Edition):

Alabsi, M. (2018). In-Flight Learning Based Flight Control of an Unmanned Aircraft System. (Thesis). University of Missouri – Kansas City. Retrieved from http://hdl.handle.net/10355/68835

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):

Alabsi, Mohammed. “In-Flight Learning Based Flight Control of an Unmanned Aircraft System.” 2018. Thesis, University of Missouri – Kansas City. Accessed March 07, 2021. http://hdl.handle.net/10355/68835.

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

MLA Handbook (7th Edition):

Alabsi, Mohammed. “In-Flight Learning Based Flight Control of an Unmanned Aircraft System.” 2018. Web. 07 Mar 2021.

Vancouver:

Alabsi M. In-Flight Learning Based Flight Control of an Unmanned Aircraft System. [Internet] [Thesis]. University of Missouri – Kansas City; 2018. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/10355/68835.

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

Council of Science Editors:

Alabsi M. In-Flight Learning Based Flight Control of an Unmanned Aircraft System. [Thesis]. University of Missouri – Kansas City; 2018. Available from: http://hdl.handle.net/10355/68835

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


Rochester Institute of Technology

14. Komendat, Andrew. Center-of-gravity estimation of an aircraft solely using traditional aircraft measurement sensors.

Degree: Mechanical Engineering, 2012, Rochester Institute of Technology

 In this work, a novel algorithm for estimating aircraft center-of-gravity location based solely on traditional aircraft measurements is investigated. The algorithm uses known physics-based kinematic… (more)

Subjects/Keywords: Aircraft; Center of gravity; Estimation; Flight dynamics; Optimization; Simulation

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APA (6th Edition):

Komendat, A. (2012). Center-of-gravity estimation of an aircraft solely using traditional aircraft measurement sensors. (Thesis). Rochester Institute of Technology. Retrieved from https://scholarworks.rit.edu/theses/195

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):

Komendat, Andrew. “Center-of-gravity estimation of an aircraft solely using traditional aircraft measurement sensors.” 2012. Thesis, Rochester Institute of Technology. Accessed March 07, 2021. https://scholarworks.rit.edu/theses/195.

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

MLA Handbook (7th Edition):

Komendat, Andrew. “Center-of-gravity estimation of an aircraft solely using traditional aircraft measurement sensors.” 2012. Web. 07 Mar 2021.

Vancouver:

Komendat A. Center-of-gravity estimation of an aircraft solely using traditional aircraft measurement sensors. [Internet] [Thesis]. Rochester Institute of Technology; 2012. [cited 2021 Mar 07]. Available from: https://scholarworks.rit.edu/theses/195.

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

Council of Science Editors:

Komendat A. Center-of-gravity estimation of an aircraft solely using traditional aircraft measurement sensors. [Thesis]. Rochester Institute of Technology; 2012. Available from: https://scholarworks.rit.edu/theses/195

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


California State University – Sacramento

15. Watt, Christian. Basic interchangeability of flight test methodology between remote controlled aircraft & full - scale aircraft.

Degree: MS, Mechanical Engineering, 2020, California State University – Sacramento

Flight test methodology is often discussed regarding full-scale aircraft, leaving out the flight testing of model aircraft. Information on how to comprehensively conduct and analyze… (more)

Subjects/Keywords: Telemetry; Flight test; RC aircraft; Sawtooth climb; Determination of airspeeds

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

APA (6th Edition):

Watt, C. (2020). Basic interchangeability of flight test methodology between remote controlled aircraft & full - scale aircraft. (Masters Thesis). California State University – Sacramento. Retrieved from http://hdl.handle.net/10211.3/217323

Chicago Manual of Style (16th Edition):

Watt, Christian. “Basic interchangeability of flight test methodology between remote controlled aircraft & full - scale aircraft.” 2020. Masters Thesis, California State University – Sacramento. Accessed March 07, 2021. http://hdl.handle.net/10211.3/217323.

MLA Handbook (7th Edition):

Watt, Christian. “Basic interchangeability of flight test methodology between remote controlled aircraft & full - scale aircraft.” 2020. Web. 07 Mar 2021.

Vancouver:

Watt C. Basic interchangeability of flight test methodology between remote controlled aircraft & full - scale aircraft. [Internet] [Masters thesis]. California State University – Sacramento; 2020. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/10211.3/217323.

Council of Science Editors:

Watt C. Basic interchangeability of flight test methodology between remote controlled aircraft & full - scale aircraft. [Masters Thesis]. California State University – Sacramento; 2020. Available from: http://hdl.handle.net/10211.3/217323


Cranfield University

16. Charpin, Jean P. F. Water flow on accreting ice surfaces.

Degree: PhD, 2002, Cranfield University

 Ice growth may rapidly degrade the aerodynamic performance of an aircraft. It can also severely damage structures such as communication towers or power lines. Subsequently,… (more)

Subjects/Keywords: 629; Aircraft icing

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APA (6th Edition):

Charpin, J. P. F. (2002). Water flow on accreting ice surfaces. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/10742 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.273526

Chicago Manual of Style (16th Edition):

Charpin, Jean P F. “Water flow on accreting ice surfaces.” 2002. Doctoral Dissertation, Cranfield University. Accessed March 07, 2021. http://dspace.lib.cranfield.ac.uk/handle/1826/10742 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.273526.

MLA Handbook (7th Edition):

Charpin, Jean P F. “Water flow on accreting ice surfaces.” 2002. Web. 07 Mar 2021.

Vancouver:

Charpin JPF. Water flow on accreting ice surfaces. [Internet] [Doctoral dissertation]. Cranfield University; 2002. [cited 2021 Mar 07]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/10742 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.273526.

Council of Science Editors:

Charpin JPF. Water flow on accreting ice surfaces. [Doctoral Dissertation]. Cranfield University; 2002. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/10742 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.273526

17. Ma, Liqun. Experimental investigations on bio-inspired surface coatings for aircraft icing mitigation.

Degree: 2019, Iowa State University

Aircraft icing is widely recognized as a significant hazard to aircraft operations in cold weathers. Bio-inspired water- and ice-phobic coatings are currently being investigated for… (more)

Subjects/Keywords: Aircraft icing; Icephobic coatings; Aerospace Engineering

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

APA (6th Edition):

Ma, L. (2019). Experimental investigations on bio-inspired surface coatings for aircraft icing mitigation. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/17053

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):

Ma, Liqun. “Experimental investigations on bio-inspired surface coatings for aircraft icing mitigation.” 2019. Thesis, Iowa State University. Accessed March 07, 2021. https://lib.dr.iastate.edu/etd/17053.

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

MLA Handbook (7th Edition):

Ma, Liqun. “Experimental investigations on bio-inspired surface coatings for aircraft icing mitigation.” 2019. Web. 07 Mar 2021.

Vancouver:

Ma L. Experimental investigations on bio-inspired surface coatings for aircraft icing mitigation. [Internet] [Thesis]. Iowa State University; 2019. [cited 2021 Mar 07]. Available from: https://lib.dr.iastate.edu/etd/17053.

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

Council of Science Editors:

Ma L. Experimental investigations on bio-inspired surface coatings for aircraft icing mitigation. [Thesis]. Iowa State University; 2019. Available from: https://lib.dr.iastate.edu/etd/17053

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


Oklahoma State University

18. Avery, Alyssa Shearon. Ice Accretion on Small Unmanned Aircraft.

Degree: Mechanical and Aerospace Engineering, 2019, Oklahoma State University

Aircraft icing is an important and complex problem. Small unmanned aerial systems are becoming increasingly common in high quality operations. The hazards of icing on… (more)

Subjects/Keywords: aircraft icing; heat transfer; unmanned systems

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APA (6th Edition):

Avery, A. S. (2019). Ice Accretion on Small Unmanned Aircraft. (Thesis). Oklahoma State University. Retrieved from http://hdl.handle.net/11244/323357

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):

Avery, Alyssa Shearon. “Ice Accretion on Small Unmanned Aircraft.” 2019. Thesis, Oklahoma State University. Accessed March 07, 2021. http://hdl.handle.net/11244/323357.

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

MLA Handbook (7th Edition):

Avery, Alyssa Shearon. “Ice Accretion on Small Unmanned Aircraft.” 2019. Web. 07 Mar 2021.

Vancouver:

Avery AS. Ice Accretion on Small Unmanned Aircraft. [Internet] [Thesis]. Oklahoma State University; 2019. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/11244/323357.

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

Council of Science Editors:

Avery AS. Ice Accretion on Small Unmanned Aircraft. [Thesis]. Oklahoma State University; 2019. Available from: http://hdl.handle.net/11244/323357

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


University of Canterbury

19. Dey, Karla. Aviation human error modelled as a production process.

Degree: Mechanical Engineering, 2015, University of Canterbury

 As technology systems have become more complex, so it is increasingly difficult for human operators to comprehend how the system is behaving. There is a… (more)

Subjects/Keywords: aircraft pilot; production process; safety; sociotechnical interaction; systems engineering; Field of Research::09 - Engineering::0901 - Aerospace Engineering::090104 - Aircraft Performance and Flight Control Systems; Field of Research::17 - Psychology and Cognitive Sciences::1702 - Cognitive Science::170202 - Decision Making

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APA (6th Edition):

Dey, K. (2015). Aviation human error modelled as a production process. (Thesis). University of Canterbury. Retrieved from http://hdl.handle.net/10092/10216

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):

Dey, Karla. “Aviation human error modelled as a production process.” 2015. Thesis, University of Canterbury. Accessed March 07, 2021. http://hdl.handle.net/10092/10216.

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

MLA Handbook (7th Edition):

Dey, Karla. “Aviation human error modelled as a production process.” 2015. Web. 07 Mar 2021.

Vancouver:

Dey K. Aviation human error modelled as a production process. [Internet] [Thesis]. University of Canterbury; 2015. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/10092/10216.

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

Council of Science Editors:

Dey K. Aviation human error modelled as a production process. [Thesis]. University of Canterbury; 2015. Available from: http://hdl.handle.net/10092/10216

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


University of Canterbury

20. Babu, Dinesh Kumar. Numerical Studies on Thrust Vectoring Using Shock- Induced Self Impinging Secondary Jets.

Degree: 2015, University of Canterbury

 Numerical studies have been carried out using a validated two-dimensional standard k-omega turbulence model for the design optimization of a thrust vector control system using… (more)

Subjects/Keywords: Fluidic thrust vectoring; rocket steering; self-impinging secondary supersonic jet; TVC in aerospace vehicles; Fields of Research::40 - Engineering::4001 - Aerospace engineering::400103 - Aircraft performance and flight control systems

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APA (6th Edition):

Babu, D. K. (2015). Numerical Studies on Thrust Vectoring Using Shock- Induced Self Impinging Secondary Jets. (Thesis). University of Canterbury. Retrieved from http://hdl.handle.net/10092/101482

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):

Babu, Dinesh Kumar. “Numerical Studies on Thrust Vectoring Using Shock- Induced Self Impinging Secondary Jets.” 2015. Thesis, University of Canterbury. Accessed March 07, 2021. http://hdl.handle.net/10092/101482.

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

MLA Handbook (7th Edition):

Babu, Dinesh Kumar. “Numerical Studies on Thrust Vectoring Using Shock- Induced Self Impinging Secondary Jets.” 2015. Web. 07 Mar 2021.

Vancouver:

Babu DK. Numerical Studies on Thrust Vectoring Using Shock- Induced Self Impinging Secondary Jets. [Internet] [Thesis]. University of Canterbury; 2015. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/10092/101482.

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

Council of Science Editors:

Babu DK. Numerical Studies on Thrust Vectoring Using Shock- Induced Self Impinging Secondary Jets. [Thesis]. University of Canterbury; 2015. Available from: http://hdl.handle.net/10092/101482

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


Linköping University

21. Martinez, Anna. Design and manufacturing of a thrust measurement system for a micro jet engine : Enabling in-flight drag estimation for subscale aircraft testing.

Degree: Fluid and Mechatronic Systems, 2018, Linköping University

  Good estimation of aerodynamic coefficients is of fundamental importance in the design and development process of an aircraft. Generally, these parameters are obtained using… (more)

Subjects/Keywords: thrust measurement; drag estimation; subscale aircraft; in-flight measurements; Engineering and Technology; Teknik och teknologier

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APA (6th Edition):

Martinez, A. (2018). Design and manufacturing of a thrust measurement system for a micro jet engine : Enabling in-flight drag estimation for subscale aircraft testing. (Thesis). Linköping University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-149288

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):

Martinez, Anna. “Design and manufacturing of a thrust measurement system for a micro jet engine : Enabling in-flight drag estimation for subscale aircraft testing.” 2018. Thesis, Linköping University. Accessed March 07, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-149288.

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

MLA Handbook (7th Edition):

Martinez, Anna. “Design and manufacturing of a thrust measurement system for a micro jet engine : Enabling in-flight drag estimation for subscale aircraft testing.” 2018. Web. 07 Mar 2021.

Vancouver:

Martinez A. Design and manufacturing of a thrust measurement system for a micro jet engine : Enabling in-flight drag estimation for subscale aircraft testing. [Internet] [Thesis]. Linköping University; 2018. [cited 2021 Mar 07]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-149288.

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

Council of Science Editors:

Martinez A. Design and manufacturing of a thrust measurement system for a micro jet engine : Enabling in-flight drag estimation for subscale aircraft testing. [Thesis]. Linköping University; 2018. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-149288

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


University of Minnesota

22. Gupta, Abhineet. Flight Dynamics Model of A Small Flexible Aircraft.

Degree: PhD, Aerospace Engineering and Mechanics, 2019, University of Minnesota

 The presence of aeroservoelastic effects in the flight dynamics of flexible aircraft presents significant challenges in terms of performance degradation and instability. In order to… (more)

Subjects/Keywords: Aeroelasticity; Flexible Aircraft; Flight Dynamics

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APA (6th Edition):

Gupta, A. (2019). Flight Dynamics Model of A Small Flexible Aircraft. (Doctoral Dissertation). University of Minnesota. Retrieved from http://hdl.handle.net/11299/211757

Chicago Manual of Style (16th Edition):

Gupta, Abhineet. “Flight Dynamics Model of A Small Flexible Aircraft.” 2019. Doctoral Dissertation, University of Minnesota. Accessed March 07, 2021. http://hdl.handle.net/11299/211757.

MLA Handbook (7th Edition):

Gupta, Abhineet. “Flight Dynamics Model of A Small Flexible Aircraft.” 2019. Web. 07 Mar 2021.

Vancouver:

Gupta A. Flight Dynamics Model of A Small Flexible Aircraft. [Internet] [Doctoral dissertation]. University of Minnesota; 2019. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/11299/211757.

Council of Science Editors:

Gupta A. Flight Dynamics Model of A Small Flexible Aircraft. [Doctoral Dissertation]. University of Minnesota; 2019. Available from: http://hdl.handle.net/11299/211757


Penn State University

23. Borigo, Cody J. A Novel Actuator Phasing Method for Ultrasonic De-icing of Aircraft Structures.

Degree: 2014, Penn State University

Aircraft icing is a critical concern for commercial and military rotorcraft and fixed-wing aircraft. In-flight icing can lead to dramatic decreases in lift and increases… (more)

Subjects/Keywords: de-icing; aircraft; ultrasound; ultrasonic; vibration; ice protection; anti-icing; phasing; piezoelectric

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

APA (6th Edition):

Borigo, C. J. (2014). A Novel Actuator Phasing Method for Ultrasonic De-icing of Aircraft Structures. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/23379

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):

Borigo, Cody J. “A Novel Actuator Phasing Method for Ultrasonic De-icing of Aircraft Structures.” 2014. Thesis, Penn State University. Accessed March 07, 2021. https://submit-etda.libraries.psu.edu/catalog/23379.

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

MLA Handbook (7th Edition):

Borigo, Cody J. “A Novel Actuator Phasing Method for Ultrasonic De-icing of Aircraft Structures.” 2014. Web. 07 Mar 2021.

Vancouver:

Borigo CJ. A Novel Actuator Phasing Method for Ultrasonic De-icing of Aircraft Structures. [Internet] [Thesis]. Penn State University; 2014. [cited 2021 Mar 07]. Available from: https://submit-etda.libraries.psu.edu/catalog/23379.

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

Council of Science Editors:

Borigo CJ. A Novel Actuator Phasing Method for Ultrasonic De-icing of Aircraft Structures. [Thesis]. Penn State University; 2014. Available from: https://submit-etda.libraries.psu.edu/catalog/23379

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


Iowa State University

24. Kolbakir, Cem. Experimental investigations on thermodynamic characteristics of DBD plasma and applications for aircraft icing mitigation.

Degree: 2019, Iowa State University

Aircraft icing is widely recognized as a significant hazard to aircraft operations. When an airplane flies in a cold climate, some of the super-cooled droplets… (more)

Subjects/Keywords: Aircraft Icing; Anti-Icing; DBD; Dielectric Barrier Discharge; Plasma Actuator; Aerospace Engineering

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

APA (6th Edition):

Kolbakir, C. (2019). Experimental investigations on thermodynamic characteristics of DBD plasma and applications for aircraft icing mitigation. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/17721

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):

Kolbakir, Cem. “Experimental investigations on thermodynamic characteristics of DBD plasma and applications for aircraft icing mitigation.” 2019. Thesis, Iowa State University. Accessed March 07, 2021. https://lib.dr.iastate.edu/etd/17721.

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

MLA Handbook (7th Edition):

Kolbakir, Cem. “Experimental investigations on thermodynamic characteristics of DBD plasma and applications for aircraft icing mitigation.” 2019. Web. 07 Mar 2021.

Vancouver:

Kolbakir C. Experimental investigations on thermodynamic characteristics of DBD plasma and applications for aircraft icing mitigation. [Internet] [Thesis]. Iowa State University; 2019. [cited 2021 Mar 07]. Available from: https://lib.dr.iastate.edu/etd/17721.

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

Council of Science Editors:

Kolbakir C. Experimental investigations on thermodynamic characteristics of DBD plasma and applications for aircraft icing mitigation. [Thesis]. Iowa State University; 2019. Available from: https://lib.dr.iastate.edu/etd/17721

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


University of Missouri – Kansas City

25. Tiemann, Christopher A. Viability and Validation of Near-Passive Descent Control for Quadrotor Systems.

Degree: 2020, University of Missouri – Kansas City

 A quadrotor unmanned aerial vehicle capable of lifting small payloads can be used to deliver small payloads from high altitudes rapidly and with high accuracy.… (more)

Subjects/Keywords: Drone aircraft; Guidance systems (Flight); Predictive control; Thesis  – University of Missouri – Kansas City  – Engineering

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APA (6th Edition):

Tiemann, C. A. (2020). Viability and Validation of Near-Passive Descent Control for Quadrotor Systems. (Thesis). University of Missouri – Kansas City. Retrieved from http://hdl.handle.net/10355/74346

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):

Tiemann, Christopher A. “Viability and Validation of Near-Passive Descent Control for Quadrotor Systems.” 2020. Thesis, University of Missouri – Kansas City. Accessed March 07, 2021. http://hdl.handle.net/10355/74346.

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

MLA Handbook (7th Edition):

Tiemann, Christopher A. “Viability and Validation of Near-Passive Descent Control for Quadrotor Systems.” 2020. Web. 07 Mar 2021.

Vancouver:

Tiemann CA. Viability and Validation of Near-Passive Descent Control for Quadrotor Systems. [Internet] [Thesis]. University of Missouri – Kansas City; 2020. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/10355/74346.

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

Council of Science Editors:

Tiemann CA. Viability and Validation of Near-Passive Descent Control for Quadrotor Systems. [Thesis]. University of Missouri – Kansas City; 2020. Available from: http://hdl.handle.net/10355/74346

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


North Carolina State University

26. Burke, David Alexander. System Level Airworthiness Tool: A Comprehensive Approach to Small Unmanned Aircraft System Airworthiness.

Degree: PhD, Aerospace Engineering, 2010, North Carolina State University

 One of the pillars of aviation safety is assuring sound engineering practices through airworthiness certification. As Unmanned Aircraft Systems (UAS) grow in popularity, the need… (more)

Subjects/Keywords: Safety Engineering; System Engineering; Point Based Tool; Unmanned Aircraft Systems; Airworthiness; Safety of Flight

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APA (6th Edition):

Burke, D. A. (2010). System Level Airworthiness Tool: A Comprehensive Approach to Small Unmanned Aircraft System Airworthiness. (Doctoral Dissertation). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/6267

Chicago Manual of Style (16th Edition):

Burke, David Alexander. “System Level Airworthiness Tool: A Comprehensive Approach to Small Unmanned Aircraft System Airworthiness.” 2010. Doctoral Dissertation, North Carolina State University. Accessed March 07, 2021. http://www.lib.ncsu.edu/resolver/1840.16/6267.

MLA Handbook (7th Edition):

Burke, David Alexander. “System Level Airworthiness Tool: A Comprehensive Approach to Small Unmanned Aircraft System Airworthiness.” 2010. Web. 07 Mar 2021.

Vancouver:

Burke DA. System Level Airworthiness Tool: A Comprehensive Approach to Small Unmanned Aircraft System Airworthiness. [Internet] [Doctoral dissertation]. North Carolina State University; 2010. [cited 2021 Mar 07]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/6267.

Council of Science Editors:

Burke DA. System Level Airworthiness Tool: A Comprehensive Approach to Small Unmanned Aircraft System Airworthiness. [Doctoral Dissertation]. North Carolina State University; 2010. Available from: http://www.lib.ncsu.edu/resolver/1840.16/6267

27. Balogh, Shelby. Use Of FOQA Data To Estimate The Probability Of Vehicle Upset Or Loss Of Control In-Flight.

Degree: MS, Aviation, 2017, University of North Dakota

  The leading cause of fatal aviation accidents worldwide remains loss of control in-flight, whereby control of the aircraft is lost or the aircraft enters… (more)

Subjects/Keywords: Aviation Safety; Loss of Control In-flight

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APA (6th Edition):

Balogh, S. (2017). Use Of FOQA Data To Estimate The Probability Of Vehicle Upset Or Loss Of Control In-Flight. (Masters Thesis). University of North Dakota. Retrieved from https://commons.und.edu/theses/2099

Chicago Manual of Style (16th Edition):

Balogh, Shelby. “Use Of FOQA Data To Estimate The Probability Of Vehicle Upset Or Loss Of Control In-Flight.” 2017. Masters Thesis, University of North Dakota. Accessed March 07, 2021. https://commons.und.edu/theses/2099.

MLA Handbook (7th Edition):

Balogh, Shelby. “Use Of FOQA Data To Estimate The Probability Of Vehicle Upset Or Loss Of Control In-Flight.” 2017. Web. 07 Mar 2021.

Vancouver:

Balogh S. Use Of FOQA Data To Estimate The Probability Of Vehicle Upset Or Loss Of Control In-Flight. [Internet] [Masters thesis]. University of North Dakota; 2017. [cited 2021 Mar 07]. Available from: https://commons.und.edu/theses/2099.

Council of Science Editors:

Balogh S. Use Of FOQA Data To Estimate The Probability Of Vehicle Upset Or Loss Of Control In-Flight. [Masters Thesis]. University of North Dakota; 2017. Available from: https://commons.und.edu/theses/2099


Brno University of Technology

28. Rydlo, Tomáš. Druhy a metody zkoušení letadel: Technics and Methods of Aircraft Testing.

Degree: 2019, Brno University of Technology

 This bachelor´s thesis deals with processing of technics and methods of aircraft testing. Even the name shows that this theme is very demanding and extensive.… (more)

Subjects/Keywords: letadla; zkoušky letadel; metody zkoušení letadel; statické zkoušky; únavové zkoušky; letové zkoušky; aircraft; aircraft test; methods of aircraft testing; static test; fatigue test; flight test

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

APA (6th Edition):

Rydlo, T. (2019). Druhy a metody zkoušení letadel: Technics and Methods of Aircraft Testing. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/10580

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):

Rydlo, Tomáš. “Druhy a metody zkoušení letadel: Technics and Methods of Aircraft Testing.” 2019. Thesis, Brno University of Technology. Accessed March 07, 2021. http://hdl.handle.net/11012/10580.

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

MLA Handbook (7th Edition):

Rydlo, Tomáš. “Druhy a metody zkoušení letadel: Technics and Methods of Aircraft Testing.” 2019. Web. 07 Mar 2021.

Vancouver:

Rydlo T. Druhy a metody zkoušení letadel: Technics and Methods of Aircraft Testing. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/11012/10580.

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

Council of Science Editors:

Rydlo T. Druhy a metody zkoušení letadel: Technics and Methods of Aircraft Testing. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/10580

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


Baylor University

29. Tecson, Joshua Logan. Convective heat transfer from realistic ice roughness distributions.

Degree: M.S.M.E., Mechanical Engineering., 2013, Baylor University

 As supercooled water droplets impinge the surfaces of in-flight aircraft, a layer of accreted ice will form. In the initial stages of the accretion process,… (more)

Subjects/Keywords: Convective heat transfer.; Aircraft icing.; Ice roughness.; Surface roughness.

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

APA (6th Edition):

Tecson, J. L. (2013). Convective heat transfer from realistic ice roughness distributions. (Masters Thesis). Baylor University. Retrieved from http://hdl.handle.net/2104/8757

Chicago Manual of Style (16th Edition):

Tecson, Joshua Logan. “Convective heat transfer from realistic ice roughness distributions.” 2013. Masters Thesis, Baylor University. Accessed March 07, 2021. http://hdl.handle.net/2104/8757.

MLA Handbook (7th Edition):

Tecson, Joshua Logan. “Convective heat transfer from realistic ice roughness distributions.” 2013. Web. 07 Mar 2021.

Vancouver:

Tecson JL. Convective heat transfer from realistic ice roughness distributions. [Internet] [Masters thesis]. Baylor University; 2013. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/2104/8757.

Council of Science Editors:

Tecson JL. Convective heat transfer from realistic ice roughness distributions. [Masters Thesis]. Baylor University; 2013. Available from: http://hdl.handle.net/2104/8757

30. Triphahn, Christopher. Lagrangian Parcel Volume method applied to icing surfaces to predict impact efficiency.

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

 When trying to predict how and where ice will accrete on an aircraft, engineers first need to be able to track the path and concentration… (more)

Subjects/Keywords: Impact Efficiency; Aircraft Icing

Aircraft icing is a major concern during the development of new aircraft components such as… …cause severe decreases in the performance, stability, and controllability of the aircraft. The… …on the surface. To better understand icing phenomena, representations of spatial and… …phase of the development process are, however, computationally intensive. Prediction… …interaction effects, such as particle collisions, coalescence, and breakup. In addition, use of the… 

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

APA (6th Edition):

Triphahn, C. (2012). Lagrangian Parcel Volume method applied to icing surfaces to predict impact efficiency. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/42376

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):

Triphahn, Christopher. “Lagrangian Parcel Volume method applied to icing surfaces to predict impact efficiency.” 2012. Thesis, University of Illinois – Urbana-Champaign. Accessed March 07, 2021. http://hdl.handle.net/2142/42376.

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

MLA Handbook (7th Edition):

Triphahn, Christopher. “Lagrangian Parcel Volume method applied to icing surfaces to predict impact efficiency.” 2012. Web. 07 Mar 2021.

Vancouver:

Triphahn C. Lagrangian Parcel Volume method applied to icing surfaces to predict impact efficiency. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2012. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/2142/42376.

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

Council of Science Editors:

Triphahn C. Lagrangian Parcel Volume method applied to icing surfaces to predict impact efficiency. [Thesis]. University of Illinois – Urbana-Champaign; 2012. Available from: http://hdl.handle.net/2142/42376

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

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