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You searched for +publisher:"Brno University of Technology" +contributor:("Popela, Robert"). Showing records 1 – 30 of 47 total matches.

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Brno University of Technology

1. Ecler, Matěj. Optimalizace vrtulí pro bezpilotní prostředky s uvážením hlučnosti: Noise reduction oriented optimization of UAV propellers.

Degree: 2020, Brno University of Technology

 This diploma thesis deals with optimization of propellers with the aim to reduce their noise level. Based on the measurement of noise level of serial… (more)

Subjects/Keywords: vrtule; akustika; intenzita hluku; turbulátor; propeller; acoustics; noise level; turbulator

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

APA (6th Edition):

Ecler, M. (2020). Optimalizace vrtulí pro bezpilotní prostředky s uvážením hlučnosti: Noise reduction oriented optimization of UAV propellers. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/192695

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):

Ecler, Matěj. “Optimalizace vrtulí pro bezpilotní prostředky s uvážením hlučnosti: Noise reduction oriented optimization of UAV propellers.” 2020. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/192695.

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

MLA Handbook (7th Edition):

Ecler, Matěj. “Optimalizace vrtulí pro bezpilotní prostředky s uvážením hlučnosti: Noise reduction oriented optimization of UAV propellers.” 2020. Web. 17 Apr 2021.

Vancouver:

Ecler M. Optimalizace vrtulí pro bezpilotní prostředky s uvážením hlučnosti: Noise reduction oriented optimization of UAV propellers. [Internet] [Thesis]. Brno University of Technology; 2020. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/192695.

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

Council of Science Editors:

Ecler M. Optimalizace vrtulí pro bezpilotní prostředky s uvážením hlučnosti: Noise reduction oriented optimization of UAV propellers. [Thesis]. Brno University of Technology; 2020. Available from: http://hdl.handle.net/11012/192695

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


Brno University of Technology

2. Pištěcká, Kateřina. Optimalizace aerodynamického odlehčení směrového kormidla letounu L-410NG: Optimization of L-410NG airplane rudder aerodynamic balance.

Degree: 2020, Brno University of Technology

The subject of this diploma thesis is a design of rudder aerodynamic balance and its optimization with regard to control forces and vertical tail and fuselage loading in critical flight modes – critical engine failure. Advisors/Committee Members: Popela, Robert (advisor), Doupník, Petr (referee).

Subjects/Keywords: vyvažovací ploška; odlehčovací ploška; aerodynamické odlehčení směrového kormidla; servo tab; trim tab; rudder aerodynamic balance

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APA (6th Edition):

Pištěcká, K. (2020). Optimalizace aerodynamického odlehčení směrového kormidla letounu L-410NG: Optimization of L-410NG airplane rudder aerodynamic balance. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/192812

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):

Pištěcká, Kateřina. “Optimalizace aerodynamického odlehčení směrového kormidla letounu L-410NG: Optimization of L-410NG airplane rudder aerodynamic balance.” 2020. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/192812.

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

MLA Handbook (7th Edition):

Pištěcká, Kateřina. “Optimalizace aerodynamického odlehčení směrového kormidla letounu L-410NG: Optimization of L-410NG airplane rudder aerodynamic balance.” 2020. Web. 17 Apr 2021.

Vancouver:

Pištěcká K. Optimalizace aerodynamického odlehčení směrového kormidla letounu L-410NG: Optimization of L-410NG airplane rudder aerodynamic balance. [Internet] [Thesis]. Brno University of Technology; 2020. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/192812.

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

Council of Science Editors:

Pištěcká K. Optimalizace aerodynamického odlehčení směrového kormidla letounu L-410NG: Optimization of L-410NG airplane rudder aerodynamic balance. [Thesis]. Brno University of Technology; 2020. Available from: http://hdl.handle.net/11012/192812

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


Brno University of Technology

3. Zíka, Jakub. Optimalizace nosiče satelitů: Small satellite dispenser structural optimization.

Degree: 2020, Brno University of Technology

 This thesis is focused on stiffness optimization of small satellite carrying structure - the Dispenser. The first chapter is an introduction to the European space… (more)

Subjects/Keywords: nosič satelitů; optimalizace; metoda konečných prvků; small satellites Dispenser; optimization; finite element method

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APA (6th Edition):

Zíka, J. (2020). Optimalizace nosiče satelitů: Small satellite dispenser structural optimization. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/193027

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):

Zíka, Jakub. “Optimalizace nosiče satelitů: Small satellite dispenser structural optimization.” 2020. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/193027.

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

MLA Handbook (7th Edition):

Zíka, Jakub. “Optimalizace nosiče satelitů: Small satellite dispenser structural optimization.” 2020. Web. 17 Apr 2021.

Vancouver:

Zíka J. Optimalizace nosiče satelitů: Small satellite dispenser structural optimization. [Internet] [Thesis]. Brno University of Technology; 2020. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/193027.

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

Council of Science Editors:

Zíka J. Optimalizace nosiče satelitů: Small satellite dispenser structural optimization. [Thesis]. Brno University of Technology; 2020. Available from: http://hdl.handle.net/11012/193027

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


Brno University of Technology

4. Havran, Edmund. Návrh konstrukce elementů předního křídla Formule Student: Design of Formula Student front wing elements.

Degree: 2020, Brno University of Technology

 The main objective of this thesis is the design of a new front wing for the Formula Student competition. The beginning of the thesis deals… (more)

Subjects/Keywords: Aerodynamika; CFD; Formula Student; Predné krídla; Prítlačné krídla; Aerodynamics; CFD; Formula Student; Front wings; Inverted wings

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APA (6th Edition):

Havran, E. (2020). Návrh konstrukce elementů předního křídla Formule Student: Design of Formula Student front wing elements. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/192549

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):

Havran, Edmund. “Návrh konstrukce elementů předního křídla Formule Student: Design of Formula Student front wing elements.” 2020. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/192549.

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

MLA Handbook (7th Edition):

Havran, Edmund. “Návrh konstrukce elementů předního křídla Formule Student: Design of Formula Student front wing elements.” 2020. Web. 17 Apr 2021.

Vancouver:

Havran E. Návrh konstrukce elementů předního křídla Formule Student: Design of Formula Student front wing elements. [Internet] [Thesis]. Brno University of Technology; 2020. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/192549.

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

Council of Science Editors:

Havran E. Návrh konstrukce elementů předního křídla Formule Student: Design of Formula Student front wing elements. [Thesis]. Brno University of Technology; 2020. Available from: http://hdl.handle.net/11012/192549

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


Brno University of Technology

5. 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 April 17, 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. 17 Apr 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 Apr 17]. 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

6. Schoř, Pavel. Použití nelineární teorie nosné čáry při aerodynamickém návrhu kluzáku: Non-linear lifting line theory application to glider aerodynamic design.

Degree: 2019, Brno University of Technology

 This master thesis shows, how can be the modified lifting line theory used for preliminary glider design an for wing loads determination. It is shown,… (more)

Subjects/Keywords: Teorie nosné čáry; kluzák; zatížení křídla; rychlostní polára; Lifting line theory; glider; wing loads; speed polar

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

APA (6th Edition):

Schoř, P. (2019). Použití nelineární teorie nosné čáry při aerodynamickém návrhu kluzáku: Non-linear lifting line theory application to glider aerodynamic design. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/3835

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):

Schoř, Pavel. “Použití nelineární teorie nosné čáry při aerodynamickém návrhu kluzáku: Non-linear lifting line theory application to glider aerodynamic design.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/3835.

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

MLA Handbook (7th Edition):

Schoř, Pavel. “Použití nelineární teorie nosné čáry při aerodynamickém návrhu kluzáku: Non-linear lifting line theory application to glider aerodynamic design.” 2019. Web. 17 Apr 2021.

Vancouver:

Schoř P. Použití nelineární teorie nosné čáry při aerodynamickém návrhu kluzáku: Non-linear lifting line theory application to glider aerodynamic design. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/3835.

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

Council of Science Editors:

Schoř P. Použití nelineární teorie nosné čáry při aerodynamickém návrhu kluzáku: Non-linear lifting line theory application to glider aerodynamic design. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/3835

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


Brno University of Technology

7. Mackovík, Matěj. Optimalizace chlazení oleje letounu VUT 100: VUT100 aircraft engine oil cooling installation optimization.

Degree: 2019, Brno University of Technology

 The mein objective of this diploma thesis is to optimize the oil cooler of the VUT 100 aircraft, so that it complies with the CS-23… (more)

Subjects/Keywords: Aerodynamika; olejový chladič; optimalizace; Ansys Fluent; VUT 100; vzduchový kanál; Aerodynamics; oil cooler; optimization; Ansys Fluent; VUT 100; air duct

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

APA (6th Edition):

Mackovík, M. (2019). Optimalizace chlazení oleje letounu VUT 100: VUT100 aircraft engine oil cooling installation optimization. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/3836

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):

Mackovík, Matěj. “Optimalizace chlazení oleje letounu VUT 100: VUT100 aircraft engine oil cooling installation optimization.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/3836.

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

MLA Handbook (7th Edition):

Mackovík, Matěj. “Optimalizace chlazení oleje letounu VUT 100: VUT100 aircraft engine oil cooling installation optimization.” 2019. Web. 17 Apr 2021.

Vancouver:

Mackovík M. Optimalizace chlazení oleje letounu VUT 100: VUT100 aircraft engine oil cooling installation optimization. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/3836.

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

Council of Science Editors:

Mackovík M. Optimalizace chlazení oleje letounu VUT 100: VUT100 aircraft engine oil cooling installation optimization. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/3836

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


Brno University of Technology

8. Pejchar, Jan. Návrh záchranného systému pro malý bezpilotní letoun: Small UAV parachute recovery system design.

Degree: 2019, Brno University of Technology

 The thesis is focused on the small UAV’s rescue system design. The thesis is divided into related sections reflecting the design process. The first part… (more)

Subjects/Keywords: Záchranný systém; padák; kritická situace; testování padáků; autopilot; vystřelovací mechanizmus; Rescue system; parachute; critical situation; parachute testing; autopilot; ejection mechanism

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APA (6th Edition):

Pejchar, J. (2019). Návrh záchranného systému pro malý bezpilotní letoun: Small UAV parachute recovery system design. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/3838

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):

Pejchar, Jan. “Návrh záchranného systému pro malý bezpilotní letoun: Small UAV parachute recovery system design.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/3838.

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

MLA Handbook (7th Edition):

Pejchar, Jan. “Návrh záchranného systému pro malý bezpilotní letoun: Small UAV parachute recovery system design.” 2019. Web. 17 Apr 2021.

Vancouver:

Pejchar J. Návrh záchranného systému pro malý bezpilotní letoun: Small UAV parachute recovery system design. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/3838.

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

Council of Science Editors:

Pejchar J. Návrh záchranného systému pro malý bezpilotní letoun: Small UAV parachute recovery system design. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/3838

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


Brno University of Technology

9. Przeczek, Jan. CFD analýza vstupního kanálu turbovrtulového motoru: CFD analysis of turboprop engine air intake.

Degree: 2019, Brno University of Technology

 This diploma thesis is focused on CFD analysis of M-601 turboprop engine nacelle mounted on L-410 commuter aircraft. Calibrating exercise is performed at the beginning… (more)

Subjects/Keywords: CFD; analýza proudění; vstupní ústrojí; motorová gondola; turbovrtulový motor M-601; letoun L-410; CFD; flow analysis; air intake; nacelle; turboprop engine M-601; aircraft L-410

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

APA (6th Edition):

Przeczek, J. (2019). CFD analýza vstupního kanálu turbovrtulového motoru: CFD analysis of turboprop engine air intake. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/3882

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):

Przeczek, Jan. “CFD analýza vstupního kanálu turbovrtulového motoru: CFD analysis of turboprop engine air intake.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/3882.

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

MLA Handbook (7th Edition):

Przeczek, Jan. “CFD analýza vstupního kanálu turbovrtulového motoru: CFD analysis of turboprop engine air intake.” 2019. Web. 17 Apr 2021.

Vancouver:

Przeczek J. CFD analýza vstupního kanálu turbovrtulového motoru: CFD analysis of turboprop engine air intake. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/3882.

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

Council of Science Editors:

Przeczek J. CFD analýza vstupního kanálu turbovrtulového motoru: CFD analysis of turboprop engine air intake. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/3882

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


Brno University of Technology

10. Koutník, Tomáš. Návrh wingletu pro kluzák LS-3: Design of winglet for LS-3 glider.

Degree: 2019, Brno University of Technology

 This diploma thesis describes the design of winglets for LS-3 glider. The method for determination of main winglet parameters based on selected criterion is presented… (more)

Subjects/Keywords: Letadlo; kluzák; winglet; křídlo; zatížení křídla; modifikace; Aircraft; glider; winglet; wing; wing loading; modification; retrofit

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

APA (6th Edition):

Koutník, T. (2019). Návrh wingletu pro kluzák LS-3: Design of winglet for LS-3 glider. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/3883

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):

Koutník, Tomáš. “Návrh wingletu pro kluzák LS-3: Design of winglet for LS-3 glider.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/3883.

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

MLA Handbook (7th Edition):

Koutník, Tomáš. “Návrh wingletu pro kluzák LS-3: Design of winglet for LS-3 glider.” 2019. Web. 17 Apr 2021.

Vancouver:

Koutník T. Návrh wingletu pro kluzák LS-3: Design of winglet for LS-3 glider. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/3883.

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

Council of Science Editors:

Koutník T. Návrh wingletu pro kluzák LS-3: Design of winglet for LS-3 glider. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/3883

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


Brno University of Technology

11. Kaňák, Ondřej. Koncepční návrh dvoumístného lehkého monitorovacího letounu: Conceptual study of light two-seater surveillance aircraft.

Degree: 2019, Brno University of Technology

 This master’s thesis deals with the conceptual design of light surveillance aircraft. It involves modifying of VUT 001 Marabu according to the new requirements, which… (more)

Subjects/Keywords: Koncepční návrh; letoun; monitorovací zařízení; letové výkony; CS – VLA; Marabu; Kondor; Conceptual study; airplane; monitoring device; flight performances; CS – VLA; Marabu; Condor

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APA (6th Edition):

Kaňák, O. (2019). Koncepční návrh dvoumístného lehkého monitorovacího letounu: Conceptual study of light two-seater surveillance aircraft. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/17204

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):

Kaňák, Ondřej. “Koncepční návrh dvoumístného lehkého monitorovacího letounu: Conceptual study of light two-seater surveillance aircraft.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/17204.

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

MLA Handbook (7th Edition):

Kaňák, Ondřej. “Koncepční návrh dvoumístného lehkého monitorovacího letounu: Conceptual study of light two-seater surveillance aircraft.” 2019. Web. 17 Apr 2021.

Vancouver:

Kaňák O. Koncepční návrh dvoumístného lehkého monitorovacího letounu: Conceptual study of light two-seater surveillance aircraft. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/17204.

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

Council of Science Editors:

Kaňák O. Koncepční návrh dvoumístného lehkého monitorovacího letounu: Conceptual study of light two-seater surveillance aircraft. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/17204

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


Brno University of Technology

12. Foltýn, Pavel. Aerodynamická analýza a optimalizace konfigurace letounu ARES: Aerodynamic analysis and shape optimization of ARES aircraft.

Degree: 2019, Brno University of Technology

 This thesis deals with the aerodynamic analysis and shape modifications of the ARES aircraft. The analysis focuses on the evaluation lift, drag, and pitching moment… (more)

Subjects/Keywords: Aerodynamická analýza; CFD; Fluent; ICEM; kalibrace CFD řešiče; sání do motoru; síť.; Aerodynamic analysis; CFD; Fluent; ICEM; calibration of the CFD solver; suction inlets; mesh.

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APA (6th Edition):

Foltýn, P. (2019). Aerodynamická analýza a optimalizace konfigurace letounu ARES: Aerodynamic analysis and shape optimization of ARES aircraft. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/40094

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. “Aerodynamická analýza a optimalizace konfigurace letounu ARES: Aerodynamic analysis and shape optimization of ARES aircraft.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/40094.

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. “Aerodynamická analýza a optimalizace konfigurace letounu ARES: Aerodynamic analysis and shape optimization of ARES aircraft.” 2019. Web. 17 Apr 2021.

Vancouver:

Foltýn P. Aerodynamická analýza a optimalizace konfigurace letounu ARES: Aerodynamic analysis and shape optimization of ARES aircraft. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/40094.

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. Aerodynamická analýza a optimalizace konfigurace letounu ARES: Aerodynamic analysis and shape optimization of ARES aircraft. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/40094

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


Brno University of Technology

13. Dolinský, Jiří. Numerická studie pulzační trysky při nízkých Reynoldsových číslech: Numerical Study Of Pulsating Jet At Moderately Small Reynolds Numbers.

Degree: 2019, Brno University of Technology

 This numerical study is focused on axisymmetric pulsatile jets of moderately small Reynolds numbers and their physics which has not been fully understood so far.… (more)

Subjects/Keywords: Proudění ve volném prostoru; trysky; úplavy; Bickleyho tryska; Schlichtingova tryska; pulzní tryska; asymptotické řešení; CFD; přímá numerická simulace.; Boundary-free shear flows; jets; wakes; mixing layers; Bickley jet; Schlichting jet; Pulsatilejet; Asymptotic solution; CFD; Direct Numerical Simulation.

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APA (6th Edition):

Dolinský, J. (2019). Numerická studie pulzační trysky při nízkých Reynoldsových číslech: Numerical Study Of Pulsating Jet At Moderately Small Reynolds Numbers. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/175532

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):

Dolinský, Jiří. “Numerická studie pulzační trysky při nízkých Reynoldsových číslech: Numerical Study Of Pulsating Jet At Moderately Small Reynolds Numbers.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/175532.

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

MLA Handbook (7th Edition):

Dolinský, Jiří. “Numerická studie pulzační trysky při nízkých Reynoldsových číslech: Numerical Study Of Pulsating Jet At Moderately Small Reynolds Numbers.” 2019. Web. 17 Apr 2021.

Vancouver:

Dolinský J. Numerická studie pulzační trysky při nízkých Reynoldsových číslech: Numerical Study Of Pulsating Jet At Moderately Small Reynolds Numbers. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/175532.

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

Council of Science Editors:

Dolinský J. Numerická studie pulzační trysky při nízkých Reynoldsových číslech: Numerical Study Of Pulsating Jet At Moderately Small Reynolds Numbers. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/175532

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


Brno University of Technology

14. Sobotka, Vojtěch. Experimentální ověření konceptu aktivního řízení proudu v automobilní aplikaci: Experimental validation of active flow control concept for automotive applications.

Degree: 2020, Brno University of Technology

 This master's thesis contains complex design of active flow control system installed on Škoda Roomster passenger car following previous research done by BUT and TUB… (more)

Subjects/Keywords: aktivní řízení proudu; osobní automobil; spoiler; snižování odporu; tlaková láhev; redukční ventil; šroubení; řezání laserem; experiment; active flow control; passenger car; spoiler; drag reduction; pressure cylinder; pressure regulator; fittings; laser cutting; experiment

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APA (6th Edition):

Sobotka, V. (2020). Experimentální ověření konceptu aktivního řízení proudu v automobilní aplikaci: Experimental validation of active flow control concept for automotive applications. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/189039

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):

Sobotka, Vojtěch. “Experimentální ověření konceptu aktivního řízení proudu v automobilní aplikaci: Experimental validation of active flow control concept for automotive applications.” 2020. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/189039.

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

MLA Handbook (7th Edition):

Sobotka, Vojtěch. “Experimentální ověření konceptu aktivního řízení proudu v automobilní aplikaci: Experimental validation of active flow control concept for automotive applications.” 2020. Web. 17 Apr 2021.

Vancouver:

Sobotka V. Experimentální ověření konceptu aktivního řízení proudu v automobilní aplikaci: Experimental validation of active flow control concept for automotive applications. [Internet] [Thesis]. Brno University of Technology; 2020. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/189039.

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

Council of Science Editors:

Sobotka V. Experimentální ověření konceptu aktivního řízení proudu v automobilní aplikaci: Experimental validation of active flow control concept for automotive applications. [Thesis]. Brno University of Technology; 2020. Available from: http://hdl.handle.net/11012/189039

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


Brno University of Technology

15. Kníř, Jakub. Parametrická studie vlivu tvaru štěrbiny mezi lopatkou rotoru turbíny a skříní motoru na aerodynamické vlastnosti rotoru: Parametric study of casing treatment for turbine blade in aero engine application.

Degree: 2018, Brno University of Technology

 This present thesis addresses the question whether it is possible to obtain compressor’s performance increase with the aid of flow numerical simulations. The main objective… (more)

Subjects/Keywords: tvarování štěrbiny skříně kompresoru; drážkování skříně; axiální kompresor; rotor 37; koncový vír; proudění ve štěrbině; casing treatment; casing grooves; axial compressor; rotor 37; tip vortex; leakage flow

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APA (6th Edition):

Kníř, J. (2018). Parametrická studie vlivu tvaru štěrbiny mezi lopatkou rotoru turbíny a skříní motoru na aerodynamické vlastnosti rotoru: Parametric study of casing treatment for turbine blade in aero engine application. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/27613

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):

Kníř, Jakub. “Parametrická studie vlivu tvaru štěrbiny mezi lopatkou rotoru turbíny a skříní motoru na aerodynamické vlastnosti rotoru: Parametric study of casing treatment for turbine blade in aero engine application.” 2018. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/27613.

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

MLA Handbook (7th Edition):

Kníř, Jakub. “Parametrická studie vlivu tvaru štěrbiny mezi lopatkou rotoru turbíny a skříní motoru na aerodynamické vlastnosti rotoru: Parametric study of casing treatment for turbine blade in aero engine application.” 2018. Web. 17 Apr 2021.

Vancouver:

Kníř J. Parametrická studie vlivu tvaru štěrbiny mezi lopatkou rotoru turbíny a skříní motoru na aerodynamické vlastnosti rotoru: Parametric study of casing treatment for turbine blade in aero engine application. [Internet] [Thesis]. Brno University of Technology; 2018. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/27613.

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

Council of Science Editors:

Kníř J. Parametrická studie vlivu tvaru štěrbiny mezi lopatkou rotoru turbíny a skříní motoru na aerodynamické vlastnosti rotoru: Parametric study of casing treatment for turbine blade in aero engine application. [Thesis]. Brno University of Technology; 2018. Available from: http://hdl.handle.net/11012/27613

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


Brno University of Technology

16. Lajza, Ondřej. Aerodynamická optimalizace návrhu trupu letounu EV 007 Sportstar: Design of Aerodynamic Optimization of Aircraft EV 007 Sportstar Fuselage.

Degree: 2019, Brno University of Technology

The diploma thesis deal with CFD based a to the aerodynamic optimalization of a fuselage and a wing fuselage junction of LSA category aircraft EV 007. Software Fluent is used. Advisors/Committee Members: Popela, Robert (advisor), Ing.Martin Drštička (referee).

Subjects/Keywords: Aerodynamika; optimalizace; CFD; Fluent; přechod křídlo trup.; Aerodynamic; optimatization; CFD; Fluent; wing fuselage junction.

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APA (6th Edition):

Lajza, O. (2019). Aerodynamická optimalizace návrhu trupu letounu EV 007 Sportstar: Design of Aerodynamic Optimization of Aircraft EV 007 Sportstar Fuselage. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/13851

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):

Lajza, Ondřej. “Aerodynamická optimalizace návrhu trupu letounu EV 007 Sportstar: Design of Aerodynamic Optimization of Aircraft EV 007 Sportstar Fuselage.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/13851.

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

MLA Handbook (7th Edition):

Lajza, Ondřej. “Aerodynamická optimalizace návrhu trupu letounu EV 007 Sportstar: Design of Aerodynamic Optimization of Aircraft EV 007 Sportstar Fuselage.” 2019. Web. 17 Apr 2021.

Vancouver:

Lajza O. Aerodynamická optimalizace návrhu trupu letounu EV 007 Sportstar: Design of Aerodynamic Optimization of Aircraft EV 007 Sportstar Fuselage. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/13851.

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

Council of Science Editors:

Lajza O. Aerodynamická optimalizace návrhu trupu letounu EV 007 Sportstar: Design of Aerodynamic Optimization of Aircraft EV 007 Sportstar Fuselage. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/13851

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


Brno University of Technology

17. Hradil, Jiří. Analýza teplotního a rychlostního pole za výstupní tryskou jednoproudového motoru: Small Jet Engine Exhaust Temperature and Velocity Flowfield Analysis.

Degree: 2019, Brno University of Technology

The diploma thesis describes search for propriate change of small jet engine exhaust, based on temperature and velocity flowfield analysis in CFD code Fluent V6. Advisors/Committee Members: Popela, Robert (advisor), Ing.Martin Babák,Ph.D. (referee).

Subjects/Keywords: CFD; proudový motor; teplotní a proudové pole; výstupní tryska; CFD; jet engine; temperature and velocity flowfield; exhaust nozzle

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APA (6th Edition):

Hradil, J. (2019). Analýza teplotního a rychlostního pole za výstupní tryskou jednoproudového motoru: Small Jet Engine Exhaust Temperature and Velocity Flowfield Analysis. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/13853

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):

Hradil, Jiří. “Analýza teplotního a rychlostního pole za výstupní tryskou jednoproudového motoru: Small Jet Engine Exhaust Temperature and Velocity Flowfield Analysis.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/13853.

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

MLA Handbook (7th Edition):

Hradil, Jiří. “Analýza teplotního a rychlostního pole za výstupní tryskou jednoproudového motoru: Small Jet Engine Exhaust Temperature and Velocity Flowfield Analysis.” 2019. Web. 17 Apr 2021.

Vancouver:

Hradil J. Analýza teplotního a rychlostního pole za výstupní tryskou jednoproudového motoru: Small Jet Engine Exhaust Temperature and Velocity Flowfield Analysis. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/13853.

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

Council of Science Editors:

Hradil J. Analýza teplotního a rychlostního pole za výstupní tryskou jednoproudového motoru: Small Jet Engine Exhaust Temperature and Velocity Flowfield Analysis. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/13853

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


Brno University of Technology

18. Vacek, Maxim. Návrh bezpilotního rotorového prostředku: Design of UAV Rotorcraft.

Degree: 2019, Brno University of Technology

 The Diploma thesis is concerned with aerodynamic designi of the ducted fan. The aim of this thesis is to compile the metod of the calculation… (more)

Subjects/Keywords: Vrtule v prstenci; bezpilotní rotorový prostředek; aerodynamický návrh.; Ducted fan; VTOL UAV; aerodynamic design.

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

APA (6th Edition):

Vacek, M. (2019). Návrh bezpilotního rotorového prostředku: Design of UAV Rotorcraft. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/14144

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):

Vacek, Maxim. “Návrh bezpilotního rotorového prostředku: Design of UAV Rotorcraft.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/14144.

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

MLA Handbook (7th Edition):

Vacek, Maxim. “Návrh bezpilotního rotorového prostředku: Design of UAV Rotorcraft.” 2019. Web. 17 Apr 2021.

Vancouver:

Vacek M. Návrh bezpilotního rotorového prostředku: Design of UAV Rotorcraft. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/14144.

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

Council of Science Editors:

Vacek M. Návrh bezpilotního rotorového prostředku: Design of UAV Rotorcraft. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/14144

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


Brno University of Technology

19. Fryšták, Lukáš. Návrh přítlačných křídel pro vůz Formule Student / SAE: Design of aerodynamic wings of Formula Student / SAE.

Degree: 2019, Brno University of Technology

 The objective of this thesis is design of aerodynamic wings for Formula Student/SAE car. Firstly, Formula Student is introduced and regulations concerning aerodynamic devices are… (more)

Subjects/Keywords: Formula Student; Aerodynamika; Přítlačná křídla; Formula Student; Aerodynamics; Inverted wings

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

APA (6th Edition):

Fryšták, L. (2019). Návrh přítlačných křídel pro vůz Formule Student / SAE: Design of aerodynamic wings of Formula Student / SAE. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/33372

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):

Fryšták, Lukáš. “Návrh přítlačných křídel pro vůz Formule Student / SAE: Design of aerodynamic wings of Formula Student / SAE.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/33372.

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

MLA Handbook (7th Edition):

Fryšták, Lukáš. “Návrh přítlačných křídel pro vůz Formule Student / SAE: Design of aerodynamic wings of Formula Student / SAE.” 2019. Web. 17 Apr 2021.

Vancouver:

Fryšták L. Návrh přítlačných křídel pro vůz Formule Student / SAE: Design of aerodynamic wings of Formula Student / SAE. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/33372.

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

Council of Science Editors:

Fryšták L. Návrh přítlačných křídel pro vůz Formule Student / SAE: Design of aerodynamic wings of Formula Student / SAE. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/33372

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


Brno University of Technology

20. Malinowski, Matěj. Aerodynamická analýza měnitelné geometrie wingletu pro aplikaci na výkonném kluzáku: Aerodynamic analysis of morphing geometry application to sailplane winglet design.

Degree: 2019, Brno University of Technology

 This master’s thesis deals with aerodynamic analysis and optimisation of sailplane winglet. Winglet is considered with ability of in-flight shape changing and optimisation process is… (more)

Subjects/Keywords: winglet; optimalizace; CFD; Computational Fluid Dynamics; adaptivní; kluzák; návrh; analýza; výkon; Winglet; optimisation; CFD; Computational Fluid Dynamics; adaptive; morphing; sailplane; glider; design; analysis; performance

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APA (6th Edition):

Malinowski, M. (2019). Aerodynamická analýza měnitelné geometrie wingletu pro aplikaci na výkonném kluzáku: Aerodynamic analysis of morphing geometry application to sailplane winglet design. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/66556

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):

Malinowski, Matěj. “Aerodynamická analýza měnitelné geometrie wingletu pro aplikaci na výkonném kluzáku: Aerodynamic analysis of morphing geometry application to sailplane winglet design.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/66556.

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

MLA Handbook (7th Edition):

Malinowski, Matěj. “Aerodynamická analýza měnitelné geometrie wingletu pro aplikaci na výkonném kluzáku: Aerodynamic analysis of morphing geometry application to sailplane winglet design.” 2019. Web. 17 Apr 2021.

Vancouver:

Malinowski M. Aerodynamická analýza měnitelné geometrie wingletu pro aplikaci na výkonném kluzáku: Aerodynamic analysis of morphing geometry application to sailplane winglet design. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/66556.

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

Council of Science Editors:

Malinowski M. Aerodynamická analýza měnitelné geometrie wingletu pro aplikaci na výkonném kluzáku: Aerodynamic analysis of morphing geometry application to sailplane winglet design. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/66556

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


Brno University of Technology

21. Navrátil, Jan. Koncepční návrh letounu VUT 001 Marabu podle předpisu CS-22: Marabu VUT 001 Aircraft Conceptual Design according to CS-22 Regulation.

Degree: 2019, Brno University of Technology

 Thesis summarizes conceptual design of VUT 001 Marabu airplane modification to fulfill CS-22 regulation requirements. Aerodynamical optimalization of wing and horizontal tail geometry is solved.… (more)

Subjects/Keywords: Koncepční návrh; VUT 001; Marabu; CS-22; Conceptual design; VUT 001; Marabu; CS-22

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

APA (6th Edition):

Navrátil, J. (2019). Koncepční návrh letounu VUT 001 Marabu podle předpisu CS-22: Marabu VUT 001 Aircraft Conceptual Design according to CS-22 Regulation. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/13850

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):

Navrátil, Jan. “Koncepční návrh letounu VUT 001 Marabu podle předpisu CS-22: Marabu VUT 001 Aircraft Conceptual Design according to CS-22 Regulation.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/13850.

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

MLA Handbook (7th Edition):

Navrátil, Jan. “Koncepční návrh letounu VUT 001 Marabu podle předpisu CS-22: Marabu VUT 001 Aircraft Conceptual Design according to CS-22 Regulation.” 2019. Web. 17 Apr 2021.

Vancouver:

Navrátil J. Koncepční návrh letounu VUT 001 Marabu podle předpisu CS-22: Marabu VUT 001 Aircraft Conceptual Design according to CS-22 Regulation. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/13850.

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

Council of Science Editors:

Navrátil J. Koncepční návrh letounu VUT 001 Marabu podle předpisu CS-22: Marabu VUT 001 Aircraft Conceptual Design according to CS-22 Regulation. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/13850

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


Brno University of Technology

22. Fenech, Daniel. Návrh výukového experimentu pro předmět Aerodynamika I: Creation of educational experiment for Aerodynamics I course.

Degree: 2019, Brno University of Technology

 The goal of this thesis is to create a semester-long project for students of the course Aerodynamics I to follow in order to understand better,… (more)

Subjects/Keywords: Aerodynamika; Aerodynamický tunel; Testování; 3D sken; Modelová letadla; P-47 Thunderbolt; XFOIL; GLAUERT III; Creo Parametric 3.0; Microsoft Excel; DEWESoft X.; Aerodynamics; Wind-Tunnel; Testing; 3D-Scan; Model Aircraft; P-47 Thunderbolt; XFOIL; GLAUERT III; Creo Parametric 3.0; Microsoft Excel; DEWESoft X.

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

APA (6th Edition):

Fenech, D. (2019). Návrh výukového experimentu pro předmět Aerodynamika I: Creation of educational experiment for Aerodynamics I course. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/176930

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):

Fenech, Daniel. “Návrh výukového experimentu pro předmět Aerodynamika I: Creation of educational experiment for Aerodynamics I course.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/176930.

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

MLA Handbook (7th Edition):

Fenech, Daniel. “Návrh výukového experimentu pro předmět Aerodynamika I: Creation of educational experiment for Aerodynamics I course.” 2019. Web. 17 Apr 2021.

Vancouver:

Fenech D. Návrh výukového experimentu pro předmět Aerodynamika I: Creation of educational experiment for Aerodynamics I course. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/176930.

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

Council of Science Editors:

Fenech D. Návrh výukového experimentu pro předmět Aerodynamika I: Creation of educational experiment for Aerodynamics I course. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/176930

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


Brno University of Technology

23. Novák, Ondřej. Předběžná aerodynamická analýza konceptu dálkově řízeného modelu s proudovým pohonem: Preliminary aerodynamic analysis of remotely controlled model with jet propulsion.

Degree: 2019, Brno University of Technology

 This bachelor´s thesis deals with aerodynamic analysis of unmanned aircraft and subsequent changes to design of wing, its position and wing-fuselage junction. In this work… (more)

Subjects/Keywords: bezpilotní; CFD; Openfoam; AVL; XFLR5; odtržení; ovladatelnost; proudový; křídlo; křídlo-trup; separace; mezní vrstva; plůtek; zub; unmanned; CFD; Openfoam; AVL; XFLR5; detachment; controllability; jet; wing; wing-fuselage junction; separation; boundary layer; fence; dog-tooth

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

APA (6th Edition):

Novák, O. (2019). Předběžná aerodynamická analýza konceptu dálkově řízeného modelu s proudovým pohonem: Preliminary aerodynamic analysis of remotely controlled model with jet propulsion. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/176931

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):

Novák, Ondřej. “Předběžná aerodynamická analýza konceptu dálkově řízeného modelu s proudovým pohonem: Preliminary aerodynamic analysis of remotely controlled model with jet propulsion.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/176931.

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

MLA Handbook (7th Edition):

Novák, Ondřej. “Předběžná aerodynamická analýza konceptu dálkově řízeného modelu s proudovým pohonem: Preliminary aerodynamic analysis of remotely controlled model with jet propulsion.” 2019. Web. 17 Apr 2021.

Vancouver:

Novák O. Předběžná aerodynamická analýza konceptu dálkově řízeného modelu s proudovým pohonem: Preliminary aerodynamic analysis of remotely controlled model with jet propulsion. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/176931.

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

Council of Science Editors:

Novák O. Předběžná aerodynamická analýza konceptu dálkově řízeného modelu s proudovým pohonem: Preliminary aerodynamic analysis of remotely controlled model with jet propulsion. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/176931

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


Brno University of Technology

24. Krmela, Luděk. Aerodyanmický návrh a výpočet kluzáku "Twin Shark": Aerodynamic design and analysis of "Twin Shark" glider.

Degree: 2019, Brno University of Technology

 The thesis contains determination of real aerodynamics characteristics of PW09-135 flap airfoil with help of calibration method via CFD, followed by accomplishment of CFD analysis… (more)

Subjects/Keywords: Twin Shark; klapkový profil PW09-135; kombinace křídlo-trup; stabilita; statická zásoba; Twin Shark; flap airfoil PW09-135; wing-fuselage junction; stability; static margin

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

APA (6th Edition):

Krmela, L. (2019). Aerodyanmický návrh a výpočet kluzáku "Twin Shark": Aerodynamic design and analysis of "Twin Shark" glider. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/1699

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):

Krmela, Luděk. “Aerodyanmický návrh a výpočet kluzáku "Twin Shark": Aerodynamic design and analysis of "Twin Shark" glider.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/1699.

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

MLA Handbook (7th Edition):

Krmela, Luděk. “Aerodyanmický návrh a výpočet kluzáku "Twin Shark": Aerodynamic design and analysis of "Twin Shark" glider.” 2019. Web. 17 Apr 2021.

Vancouver:

Krmela L. Aerodyanmický návrh a výpočet kluzáku "Twin Shark": Aerodynamic design and analysis of "Twin Shark" glider. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/1699.

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

Council of Science Editors:

Krmela L. Aerodyanmický návrh a výpočet kluzáku "Twin Shark": Aerodynamic design and analysis of "Twin Shark" glider. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/1699

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


Brno University of Technology

25. Kubíček, Martin. Aerodynamická optimalizace karoserie automobilu: Aerodynamic optimization of passenger car body.

Degree: 2019, Brno University of Technology

The diploma thesis is focused on create an optimization methodology for CFD issues or any other computationally demanding software. Optimization method is applied on simplified model of car, where improves its aerodynamic properties Advisors/Committee Members: Popela, Robert (advisor), Fiľakovský, Karol (referee).

Subjects/Keywords: Optimalizace; multiobjektová optimalizace; karosérie vozu; uniformní design; citlivostní analýza; CFD; Krigingův metamodel; Optimization; multiobject optimization; body car; uniform design; sensitivity analysis; CFD; Kriging metamodel

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

APA (6th Edition):

Kubíček, M. (2019). Aerodynamická optimalizace karoserie automobilu: Aerodynamic optimization of passenger car body. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/1700

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):

Kubíček, Martin. “Aerodynamická optimalizace karoserie automobilu: Aerodynamic optimization of passenger car body.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/1700.

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

MLA Handbook (7th Edition):

Kubíček, Martin. “Aerodynamická optimalizace karoserie automobilu: Aerodynamic optimization of passenger car body.” 2019. Web. 17 Apr 2021.

Vancouver:

Kubíček M. Aerodynamická optimalizace karoserie automobilu: Aerodynamic optimization of passenger car body. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/1700.

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

Council of Science Editors:

Kubíček M. Aerodynamická optimalizace karoserie automobilu: Aerodynamic optimization of passenger car body. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/1700

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


Brno University of Technology

26. Dvořák, Petr. Optimalizace štěrbinové vztlakové klapky letounu: Optimization of single slotted flap.

Degree: 2019, Brno University of Technology

 The main objective of this diploma thesis is to optimize the high lift device on the wing of the Phoenix Air U-15 ultralight aircraft, so… (more)

Subjects/Keywords: Aerodynamika; optimalizace; metoda plochy odezvy; vysokovztlaký systém; štěrbinová vztlaková klapka; profil SM 701; kalibrace GA(W) – 2; CFD; Ansys Fluent v6; Aerodynamics; optimization; Response Surface Method; high-lift device; slotted flap; SM 701 airfoil; GA(W) – 2 airfoil calibration; CFD; Ansys Fluent v6

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

APA (6th Edition):

Dvořák, P. (2019). Optimalizace štěrbinové vztlakové klapky letounu: Optimization of single slotted flap. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/13421

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):

Dvořák, Petr. “Optimalizace štěrbinové vztlakové klapky letounu: Optimization of single slotted flap.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/13421.

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

MLA Handbook (7th Edition):

Dvořák, Petr. “Optimalizace štěrbinové vztlakové klapky letounu: Optimization of single slotted flap.” 2019. Web. 17 Apr 2021.

Vancouver:

Dvořák P. Optimalizace štěrbinové vztlakové klapky letounu: Optimization of single slotted flap. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/13421.

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

Council of Science Editors:

Dvořák P. Optimalizace štěrbinové vztlakové klapky letounu: Optimization of single slotted flap. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/13421

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


Brno University of Technology

27. Matěják, Vladimír. Návrh letounu VUT 022 s proudovým pohonem dle předpisu CS-22: Design VUT 022 Aircraft with Jet Engine according to CS-22 Regulation.

Degree: 2019, Brno University of Technology

 The diploma thesis deals with the design, load calculation and stress analysis of a composite wing construction of an airplane based on the construction of… (more)

Subjects/Keywords: VUT 001 Marabu; křídlo; zatížení; kompozit; proudový motor; VUT 001 Marabu; wing; load; composite; jet engine

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

APA (6th Edition):

Matěják, V. (2019). Návrh letounu VUT 022 s proudovým pohonem dle předpisu CS-22: Design VUT 022 Aircraft with Jet Engine according to CS-22 Regulation. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/9913

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):

Matěják, Vladimír. “Návrh letounu VUT 022 s proudovým pohonem dle předpisu CS-22: Design VUT 022 Aircraft with Jet Engine according to CS-22 Regulation.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/9913.

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

MLA Handbook (7th Edition):

Matěják, Vladimír. “Návrh letounu VUT 022 s proudovým pohonem dle předpisu CS-22: Design VUT 022 Aircraft with Jet Engine according to CS-22 Regulation.” 2019. Web. 17 Apr 2021.

Vancouver:

Matěják V. Návrh letounu VUT 022 s proudovým pohonem dle předpisu CS-22: Design VUT 022 Aircraft with Jet Engine according to CS-22 Regulation. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/9913.

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

Council of Science Editors:

Matěják V. Návrh letounu VUT 022 s proudovým pohonem dle předpisu CS-22: Design VUT 022 Aircraft with Jet Engine according to CS-22 Regulation. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/9913

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


Brno University of Technology

28. Fryšták, Lukáš. Aerodynamická optimalizace monopostu formule SAE: Formula SAE aerodynamic optimization.

Degree: 2019, Brno University of Technology

 This work focuses on wind tunnel testing of a 25% scale model of a Formula SAE race car. In the first part, Formula SAE competition… (more)

Subjects/Keywords: Formula SAE; Formula Student; aerodynamický tunel; aerodynamika; tenzometrická váha; Formula SAE; Formula Student; Wind tunnel; aerodynamics; force balance

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

APA (6th Edition):

Fryšták, L. (2019). Aerodynamická optimalizace monopostu formule SAE: Formula SAE aerodynamic optimization. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/60795

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):

Fryšták, Lukáš. “Aerodynamická optimalizace monopostu formule SAE: Formula SAE aerodynamic optimization.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/60795.

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

MLA Handbook (7th Edition):

Fryšták, Lukáš. “Aerodynamická optimalizace monopostu formule SAE: Formula SAE aerodynamic optimization.” 2019. Web. 17 Apr 2021.

Vancouver:

Fryšták L. Aerodynamická optimalizace monopostu formule SAE: Formula SAE aerodynamic optimization. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/60795.

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

Council of Science Editors:

Fryšták L. Aerodynamická optimalizace monopostu formule SAE: Formula SAE aerodynamic optimization. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/60795

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


Brno University of Technology

29. Fojtl, Michal. Výpočet aerodynamických charakteristik nosiče pro nízkou oběžnou dráhu: Aerodynamic analysis of low orbit launcher.

Degree: 2019, Brno University of Technology

 Master’s thesis deals with aerodynamic heating of launch vehicle during ascent phase by using CFD simulation. Ascent trajectory and payload fairing geometry is design using… (more)

Subjects/Keywords: Aerodynamický ohřev; CFD; nosné rakety; nadzvukové proudění; hypersonické proudění; štíhlá tělesa; osově symetrická tělesa; Aerodynamic heating; CFD; launch vehicles; supersonic flow; hypersonic flow; slender bodies; bodies of revolution

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

APA (6th Edition):

Fojtl, M. (2019). Výpočet aerodynamických charakteristik nosiče pro nízkou oběžnou dráhu: Aerodynamic analysis of low orbit launcher. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/65550

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):

Fojtl, Michal. “Výpočet aerodynamických charakteristik nosiče pro nízkou oběžnou dráhu: Aerodynamic analysis of low orbit launcher.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/65550.

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

MLA Handbook (7th Edition):

Fojtl, Michal. “Výpočet aerodynamických charakteristik nosiče pro nízkou oběžnou dráhu: Aerodynamic analysis of low orbit launcher.” 2019. Web. 17 Apr 2021.

Vancouver:

Fojtl M. Výpočet aerodynamických charakteristik nosiče pro nízkou oběžnou dráhu: Aerodynamic analysis of low orbit launcher. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/65550.

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

Council of Science Editors:

Fojtl M. Výpočet aerodynamických charakteristik nosiče pro nízkou oběžnou dráhu: Aerodynamic analysis of low orbit launcher. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/65550

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


Brno University of Technology

30. Jánošík, Tomáš. Aerodynamická analýza prototypu létajícího automobilu Aircar 5.0: Aerodynamic analysis of the Aircar 5.0 flying car prototype.

Degree: 2019, Brno University of Technology

 This thesis focuses on CFD analysis of the Aircar 5.0 flying car prototype. The theoretical part covers basic information about the connection between the aerodynamics… (more)

Subjects/Keywords: aerodynamika; prúdenie; CFD; lietajúci automobil; aerodynamics; airflow; CFD; flying car

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

APA (6th Edition):

Jánošík, T. (2019). Aerodynamická analýza prototypu létajícího automobilu Aircar 5.0: Aerodynamic analysis of the Aircar 5.0 flying car prototype. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/175528

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):

Jánošík, Tomáš. “Aerodynamická analýza prototypu létajícího automobilu Aircar 5.0: Aerodynamic analysis of the Aircar 5.0 flying car prototype.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/175528.

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

MLA Handbook (7th Edition):

Jánošík, Tomáš. “Aerodynamická analýza prototypu létajícího automobilu Aircar 5.0: Aerodynamic analysis of the Aircar 5.0 flying car prototype.” 2019. Web. 17 Apr 2021.

Vancouver:

Jánošík T. Aerodynamická analýza prototypu létajícího automobilu Aircar 5.0: Aerodynamic analysis of the Aircar 5.0 flying car prototype. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/175528.

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

Council of Science Editors:

Jánošík T. Aerodynamická analýza prototypu létajícího automobilu Aircar 5.0: Aerodynamic analysis of the Aircar 5.0 flying car prototype. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/175528

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

[1] [2]

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