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You searched for subject:(drag due to lift). Showing records 1 – 30 of 28738 total matches.

[1] [2] [3] [4] [5] … [958]

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Brno University of Technology

1. Skarolek, Vilém. Možnosti minimalizace indukovaného odporu: Possibilities of minimalization of induced drag.

Degree: 2019, Brno University of Technology

Lift-induced drag is a significant part of total drag of airplane during flight, thus its minimization is desirable for economical operation of air service. This… (more)

Subjects/Keywords: minimalizace; indukovaný odpor; aerodynamika; winglety; minimalization; induced drag; drag due to lift; aerodynamics; winglet

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APA (6th Edition):

Skarolek, V. (2019). Možnosti minimalizace indukovaného odporu: Possibilities of minimalization of induced drag. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/2222

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):

Skarolek, Vilém. “Možnosti minimalizace indukovaného odporu: Possibilities of minimalization of induced drag.” 2019. Thesis, Brno University of Technology. Accessed January 24, 2021. http://hdl.handle.net/11012/2222.

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

MLA Handbook (7th Edition):

Skarolek, Vilém. “Možnosti minimalizace indukovaného odporu: Possibilities of minimalization of induced drag.” 2019. Web. 24 Jan 2021.

Vancouver:

Skarolek V. Možnosti minimalizace indukovaného odporu: Possibilities of minimalization of induced drag. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/11012/2222.

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

Council of Science Editors:

Skarolek V. Možnosti minimalizace indukovaného odporu: Possibilities of minimalization of induced drag. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/2222

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


Brigham Young University

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

Degree: MS, 2003, Brigham Young University

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Luke, Mark Elden. “Predicting Drag Polars For Micro Air Vehicles.” 2003. Masters Thesis, Brigham Young University. Accessed January 24, 2021. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1107&context=etd.

MLA Handbook (7th Edition):

Luke, Mark Elden. “Predicting Drag Polars For Micro Air Vehicles.” 2003. Web. 24 Jan 2021.

Vancouver:

Luke ME. Predicting Drag Polars For Micro Air Vehicles. [Internet] [Masters thesis]. Brigham Young University; 2003. [cited 2021 Jan 24]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1107&context=etd.

Council of Science Editors:

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


University of Dayton

3. Goodman, Steven Blake. Correlations Between Near Wake Velocity Fluctuations and Aerodynamic Efficiency for the SD7003 Airfoil.

Degree: MS(M.S.), Aerospace Engineering, 2018, University of Dayton

 The correlation in turbulent properties between the near wake, far wake and aerodynamic efficiency has not been explored so far. Overall, the goal of this… (more)

Subjects/Keywords: Aerospace Engineering; Fluid Dynamics; Turbulence; aerodynamic efficiency; SD7003; velocity flucations; lift-to-drag ratio; aerodynamics

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APA (6th Edition):

Goodman, S. B. (2018). Correlations Between Near Wake Velocity Fluctuations and Aerodynamic Efficiency for the SD7003 Airfoil. (Masters Thesis). University of Dayton. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=dayton1524137507116155

Chicago Manual of Style (16th Edition):

Goodman, Steven Blake. “Correlations Between Near Wake Velocity Fluctuations and Aerodynamic Efficiency for the SD7003 Airfoil.” 2018. Masters Thesis, University of Dayton. Accessed January 24, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1524137507116155.

MLA Handbook (7th Edition):

Goodman, Steven Blake. “Correlations Between Near Wake Velocity Fluctuations and Aerodynamic Efficiency for the SD7003 Airfoil.” 2018. Web. 24 Jan 2021.

Vancouver:

Goodman SB. Correlations Between Near Wake Velocity Fluctuations and Aerodynamic Efficiency for the SD7003 Airfoil. [Internet] [Masters thesis]. University of Dayton; 2018. [cited 2021 Jan 24]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1524137507116155.

Council of Science Editors:

Goodman SB. Correlations Between Near Wake Velocity Fluctuations and Aerodynamic Efficiency for the SD7003 Airfoil. [Masters Thesis]. University of Dayton; 2018. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1524137507116155


University of Vermont

4. Newman, Dante M. Lift & Drag Effects of a Variable-Angle Winglet System.

Degree: Mechanical Engineering, 2020, University of Vermont

  Winglets are systems that are used on aircraft to reduce drag and ultimately save money on fuel and pollution costs. A winglet exists on… (more)

Subjects/Keywords: Winglet; Angle; Wing; Drag; Lift; CFD

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APA (6th Edition):

Newman, D. M. (2020). Lift & Drag Effects of a Variable-Angle Winglet System. (Thesis). University of Vermont. Retrieved from https://scholarworks.uvm.edu/hcoltheses/356

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):

Newman, Dante M. “Lift & Drag Effects of a Variable-Angle Winglet System.” 2020. Thesis, University of Vermont. Accessed January 24, 2021. https://scholarworks.uvm.edu/hcoltheses/356.

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

MLA Handbook (7th Edition):

Newman, Dante M. “Lift & Drag Effects of a Variable-Angle Winglet System.” 2020. Web. 24 Jan 2021.

Vancouver:

Newman DM. Lift & Drag Effects of a Variable-Angle Winglet System. [Internet] [Thesis]. University of Vermont; 2020. [cited 2021 Jan 24]. Available from: https://scholarworks.uvm.edu/hcoltheses/356.

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

Council of Science Editors:

Newman DM. Lift & Drag Effects of a Variable-Angle Winglet System. [Thesis]. University of Vermont; 2020. Available from: https://scholarworks.uvm.edu/hcoltheses/356

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


Utah State University

5. Stewart, Austin J. Impact of Parasitic Drag on a Family of Optimal Lift Distributions.

Degree: MS, Mechanical and Aerospace Engineering, 2020, Utah State University

  Minimizing drag is a variational problem, and several minimum induced drag solutions have been found using different design constraints. The elliptic lift distribution is… (more)

Subjects/Keywords: Induced Drag; Parasitic Drag; Lift Distribution; Lifting Line Theory; Reducing Drag; Aerospace Engineering

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

APA (6th Edition):

Stewart, A. J. (2020). Impact of Parasitic Drag on a Family of Optimal Lift Distributions. (Masters Thesis). Utah State University. Retrieved from https://digitalcommons.usu.edu/etd/7740

Chicago Manual of Style (16th Edition):

Stewart, Austin J. “Impact of Parasitic Drag on a Family of Optimal Lift Distributions.” 2020. Masters Thesis, Utah State University. Accessed January 24, 2021. https://digitalcommons.usu.edu/etd/7740.

MLA Handbook (7th Edition):

Stewart, Austin J. “Impact of Parasitic Drag on a Family of Optimal Lift Distributions.” 2020. Web. 24 Jan 2021.

Vancouver:

Stewart AJ. Impact of Parasitic Drag on a Family of Optimal Lift Distributions. [Internet] [Masters thesis]. Utah State University; 2020. [cited 2021 Jan 24]. Available from: https://digitalcommons.usu.edu/etd/7740.

Council of Science Editors:

Stewart AJ. Impact of Parasitic Drag on a Family of Optimal Lift Distributions. [Masters Thesis]. Utah State University; 2020. Available from: https://digitalcommons.usu.edu/etd/7740


Delft University of Technology

6. Kinderman, Hendrik Wisse (author). The impact of vertical wing placement on the wave drag and sonic-boom performance at supersonic speeds.

Degree: 2017, Delft University of Technology

 This research project aims at obtaining a better understanding of vertically translating the wing and the related wing-body interference effects on the drag and sonic… (more)

Subjects/Keywords: sonic boom; vertical wing placement; wave drag; drag; supersonic; pressure signature; lift; zero-lift; area ruling; area rule; Mach; cone

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APA (6th Edition):

Kinderman, H. W. (. (2017). The impact of vertical wing placement on the wave drag and sonic-boom performance at supersonic speeds. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:b5eaa808-6067-46a5-8d45-0e14d18ceeef

Chicago Manual of Style (16th Edition):

Kinderman, Hendrik Wisse (author). “The impact of vertical wing placement on the wave drag and sonic-boom performance at supersonic speeds.” 2017. Masters Thesis, Delft University of Technology. Accessed January 24, 2021. http://resolver.tudelft.nl/uuid:b5eaa808-6067-46a5-8d45-0e14d18ceeef.

MLA Handbook (7th Edition):

Kinderman, Hendrik Wisse (author). “The impact of vertical wing placement on the wave drag and sonic-boom performance at supersonic speeds.” 2017. Web. 24 Jan 2021.

Vancouver:

Kinderman HW(. The impact of vertical wing placement on the wave drag and sonic-boom performance at supersonic speeds. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 24]. Available from: http://resolver.tudelft.nl/uuid:b5eaa808-6067-46a5-8d45-0e14d18ceeef.

Council of Science Editors:

Kinderman HW(. The impact of vertical wing placement on the wave drag and sonic-boom performance at supersonic speeds. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:b5eaa808-6067-46a5-8d45-0e14d18ceeef


Delft University of Technology

7. Naderi, Nader (author). Numerical Simulation of Hydrodynamic Forces on Bridge Decks.

Degree: 2018, Delft University of Technology

 Highway bridges along the coast and small river bridges in mountainous regions can be submerged during storm surges or strong rainfall events, respectively. Loss of… (more)

Subjects/Keywords: CoMEM; Fluent; hydrodynamic forces; bridge deck; drag; lift; moment; numerical simulation

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

APA (6th Edition):

Naderi, N. (. (2018). Numerical Simulation of Hydrodynamic Forces on Bridge Decks. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:3605d7b8-8315-4469-81da-d1c0bfdb23fb

Chicago Manual of Style (16th Edition):

Naderi, Nader (author). “Numerical Simulation of Hydrodynamic Forces on Bridge Decks.” 2018. Masters Thesis, Delft University of Technology. Accessed January 24, 2021. http://resolver.tudelft.nl/uuid:3605d7b8-8315-4469-81da-d1c0bfdb23fb.

MLA Handbook (7th Edition):

Naderi, Nader (author). “Numerical Simulation of Hydrodynamic Forces on Bridge Decks.” 2018. Web. 24 Jan 2021.

Vancouver:

Naderi N(. Numerical Simulation of Hydrodynamic Forces on Bridge Decks. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Jan 24]. Available from: http://resolver.tudelft.nl/uuid:3605d7b8-8315-4469-81da-d1c0bfdb23fb.

Council of Science Editors:

Naderi N(. Numerical Simulation of Hydrodynamic Forces on Bridge Decks. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:3605d7b8-8315-4469-81da-d1c0bfdb23fb


Virginia Tech

8. Larson, Christopher Whitford. The Design and Construction of a 20" x 20" Mach 2.0 Blowdown Wind Tunnel to Characterize the Lift and Drag of Irregularly Shaped Fragments.

Degree: MS, Mechanical Engineering, 2011, Virginia Tech

 A supersonic wind tunnel, with a 20" x 20'" test section cross sectional area, was designed and constructed at the Techsburg Wind Tunnel Facility in… (more)

Subjects/Keywords: Irregularly Shaped Fragments; Lift and Drag Force; Supersonic Wind Tunnel

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

APA (6th Edition):

Larson, C. W. (2011). The Design and Construction of a 20" x 20" Mach 2.0 Blowdown Wind Tunnel to Characterize the Lift and Drag of Irregularly Shaped Fragments. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/76968

Chicago Manual of Style (16th Edition):

Larson, Christopher Whitford. “The Design and Construction of a 20" x 20" Mach 2.0 Blowdown Wind Tunnel to Characterize the Lift and Drag of Irregularly Shaped Fragments.” 2011. Masters Thesis, Virginia Tech. Accessed January 24, 2021. http://hdl.handle.net/10919/76968.

MLA Handbook (7th Edition):

Larson, Christopher Whitford. “The Design and Construction of a 20" x 20" Mach 2.0 Blowdown Wind Tunnel to Characterize the Lift and Drag of Irregularly Shaped Fragments.” 2011. Web. 24 Jan 2021.

Vancouver:

Larson CW. The Design and Construction of a 20" x 20" Mach 2.0 Blowdown Wind Tunnel to Characterize the Lift and Drag of Irregularly Shaped Fragments. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/10919/76968.

Council of Science Editors:

Larson CW. The Design and Construction of a 20" x 20" Mach 2.0 Blowdown Wind Tunnel to Characterize the Lift and Drag of Irregularly Shaped Fragments. [Masters Thesis]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/76968


University of Alberta

9. AlGendy,Mohammad. Acceleration due to gravity on a rapidly rotating neutron star.

Degree: MS, Department of Physics, 2012, University of Alberta

 In this thesis I am going to calculate the acceleration due to gravity on axisymmetric neutron stars using the rapidly rotating neutron star code (RNS).… (more)

Subjects/Keywords: Rotating neutron star; Acceleration due to gravity

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APA (6th Edition):

AlGendy,Mohammad. (2012). Acceleration due to gravity on a rapidly rotating neutron star. (Masters Thesis). University of Alberta. Retrieved from https://era.library.ualberta.ca/files/9g54xj73t

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Chicago Manual of Style (16th Edition):

AlGendy,Mohammad. “Acceleration due to gravity on a rapidly rotating neutron star.” 2012. Masters Thesis, University of Alberta. Accessed January 24, 2021. https://era.library.ualberta.ca/files/9g54xj73t.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

MLA Handbook (7th Edition):

AlGendy,Mohammad. “Acceleration due to gravity on a rapidly rotating neutron star.” 2012. Web. 24 Jan 2021.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Vancouver:

AlGendy,Mohammad. Acceleration due to gravity on a rapidly rotating neutron star. [Internet] [Masters thesis]. University of Alberta; 2012. [cited 2021 Jan 24]. Available from: https://era.library.ualberta.ca/files/9g54xj73t.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Council of Science Editors:

AlGendy,Mohammad. Acceleration due to gravity on a rapidly rotating neutron star. [Masters Thesis]. University of Alberta; 2012. Available from: https://era.library.ualberta.ca/files/9g54xj73t

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete


Cranfield University

10. Sibilli, Thierry. Modelling the aerodynamics of propulsive system integration at cruise and high-lift conditions.

Degree: PhD, 2012, Cranfield University

Due to a trend towards Ultra High Bypass Ratio engines the corresponding engine/airframe interference is becoming a key aspect in aircraft design. The present economic… (more)

Subjects/Keywords: Engine-Airframe Interaction; Net Propulsive Force; High-Lift CFD; High-lift Installation Vortex; Nacelle chine; Drag Extraction

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

APA (6th Edition):

Sibilli, T. (2012). Modelling the aerodynamics of propulsive system integration at cruise and high-lift conditions. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/7945

Chicago Manual of Style (16th Edition):

Sibilli, Thierry. “Modelling the aerodynamics of propulsive system integration at cruise and high-lift conditions.” 2012. Doctoral Dissertation, Cranfield University. Accessed January 24, 2021. http://dspace.lib.cranfield.ac.uk/handle/1826/7945.

MLA Handbook (7th Edition):

Sibilli, Thierry. “Modelling the aerodynamics of propulsive system integration at cruise and high-lift conditions.” 2012. Web. 24 Jan 2021.

Vancouver:

Sibilli T. Modelling the aerodynamics of propulsive system integration at cruise and high-lift conditions. [Internet] [Doctoral dissertation]. Cranfield University; 2012. [cited 2021 Jan 24]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/7945.

Council of Science Editors:

Sibilli T. Modelling the aerodynamics of propulsive system integration at cruise and high-lift conditions. [Doctoral Dissertation]. Cranfield University; 2012. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/7945


Cranfield University

11. Sibilli, Thierry. Modelling the aerodynamics of propulsive system integration at cruise and high-lift conditions.

Degree: PhD, 2012, Cranfield University

Due to a trend towards Ultra High Bypass Ratio engines the corresponding engine/airframe interference is becoming a key aspect in aircraft design. The present economic… (more)

Subjects/Keywords: 629.132; Engine-Airframe Interaction; Net Propulsive Force; High-Lift CFD; High-lift Installation Vortex; Nacelle chine; Drag Extraction

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

APA (6th Edition):

Sibilli, T. (2012). Modelling the aerodynamics of propulsive system integration at cruise and high-lift conditions. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/7945 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.573646

Chicago Manual of Style (16th Edition):

Sibilli, Thierry. “Modelling the aerodynamics of propulsive system integration at cruise and high-lift conditions.” 2012. Doctoral Dissertation, Cranfield University. Accessed January 24, 2021. http://dspace.lib.cranfield.ac.uk/handle/1826/7945 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.573646.

MLA Handbook (7th Edition):

Sibilli, Thierry. “Modelling the aerodynamics of propulsive system integration at cruise and high-lift conditions.” 2012. Web. 24 Jan 2021.

Vancouver:

Sibilli T. Modelling the aerodynamics of propulsive system integration at cruise and high-lift conditions. [Internet] [Doctoral dissertation]. Cranfield University; 2012. [cited 2021 Jan 24]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/7945 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.573646.

Council of Science Editors:

Sibilli T. Modelling the aerodynamics of propulsive system integration at cruise and high-lift conditions. [Doctoral Dissertation]. Cranfield University; 2012. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/7945 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.573646


RMIT University

12. Moria, H. Experimental study of aerodynamic behaviour of stretchable sport fabrics.

Degree: 2013, RMIT University

 In recent years, there has been great interest in the effects of different garments and their aerodynamic characteristics. It is widely believed that the reduction… (more)

Subjects/Keywords: Fields of Research; Aerodynamics; sports garments; drag; lift; wind tunnel; surface morphology

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APA (6th Edition):

Moria, H. (2013). Experimental study of aerodynamic behaviour of stretchable sport fabrics. (Thesis). RMIT University. Retrieved from http://researchbank.rmit.edu.au/view/rmit:160467

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):

Moria, H. “Experimental study of aerodynamic behaviour of stretchable sport fabrics.” 2013. Thesis, RMIT University. Accessed January 24, 2021. http://researchbank.rmit.edu.au/view/rmit:160467.

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

MLA Handbook (7th Edition):

Moria, H. “Experimental study of aerodynamic behaviour of stretchable sport fabrics.” 2013. Web. 24 Jan 2021.

Vancouver:

Moria H. Experimental study of aerodynamic behaviour of stretchable sport fabrics. [Internet] [Thesis]. RMIT University; 2013. [cited 2021 Jan 24]. Available from: http://researchbank.rmit.edu.au/view/rmit:160467.

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

Council of Science Editors:

Moria H. Experimental study of aerodynamic behaviour of stretchable sport fabrics. [Thesis]. RMIT University; 2013. Available from: http://researchbank.rmit.edu.au/view/rmit:160467

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


RMIT University

13. Mavuri, S. Aerodynamic analysis of vehicle wheel-housings.

Degree: 2009, RMIT University

 Aerodynamics has a strong influence on the design of a vehicle. Over half the fuel used by modern passenger is wasted in overcoming aerodynamic drag.… (more)

Subjects/Keywords: Fields of Research; vehicle; aerodynamics; wheel housing; wheel-well; drag; lift; double symmetry

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APA (6th Edition):

Mavuri, S. (2009). Aerodynamic analysis of vehicle wheel-housings. (Thesis). RMIT University. Retrieved from http://researchbank.rmit.edu.au/view/rmit:161794

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):

Mavuri, S. “Aerodynamic analysis of vehicle wheel-housings.” 2009. Thesis, RMIT University. Accessed January 24, 2021. http://researchbank.rmit.edu.au/view/rmit:161794.

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

MLA Handbook (7th Edition):

Mavuri, S. “Aerodynamic analysis of vehicle wheel-housings.” 2009. Web. 24 Jan 2021.

Vancouver:

Mavuri S. Aerodynamic analysis of vehicle wheel-housings. [Internet] [Thesis]. RMIT University; 2009. [cited 2021 Jan 24]. Available from: http://researchbank.rmit.edu.au/view/rmit:161794.

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

Council of Science Editors:

Mavuri S. Aerodynamic analysis of vehicle wheel-housings. [Thesis]. RMIT University; 2009. Available from: http://researchbank.rmit.edu.au/view/rmit:161794

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


Universidade do Rio Grande do Sul

14. Gomes, Lara Elena. Comparação entre forças propulsivas efetivas calculadas e medida durante um palmateio de sustentação.

Degree: 2010, Universidade do Rio Grande do Sul

A força propulsiva gerada durante o palmateio é resultado do somatório das forças de arrasto e de sustentação, sendo que a componente que atua na… (more)

Subjects/Keywords: Propulsion; Biomecânica; Attack angle; Natação : Fisiologia; Força; Drag force; Lift force; Swimming; Synchronized swimming

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APA (6th Edition):

Gomes, L. E. (2010). Comparação entre forças propulsivas efetivas calculadas e medida durante um palmateio de sustentação. (Thesis). Universidade do Rio Grande do Sul. Retrieved from http://hdl.handle.net/10183/27677

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):

Gomes, Lara Elena. “Comparação entre forças propulsivas efetivas calculadas e medida durante um palmateio de sustentação.” 2010. Thesis, Universidade do Rio Grande do Sul. Accessed January 24, 2021. http://hdl.handle.net/10183/27677.

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

MLA Handbook (7th Edition):

Gomes, Lara Elena. “Comparação entre forças propulsivas efetivas calculadas e medida durante um palmateio de sustentação.” 2010. Web. 24 Jan 2021.

Vancouver:

Gomes LE. Comparação entre forças propulsivas efetivas calculadas e medida durante um palmateio de sustentação. [Internet] [Thesis]. Universidade do Rio Grande do Sul; 2010. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/10183/27677.

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

Council of Science Editors:

Gomes LE. Comparação entre forças propulsivas efetivas calculadas e medida durante um palmateio de sustentação. [Thesis]. Universidade do Rio Grande do Sul; 2010. Available from: http://hdl.handle.net/10183/27677

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

15. Araujo Filho, Maurilio Messias de. Efeito da variação de câmber nas características aerodinâmicas de uma asa tri-dimensional.

Degree: Mestrado, Aeronaves, 2008, University of São Paulo

O presente trabalho tem por finalidade a obtenção de curvas que regem o comportamento estático da sustentação e arrasto de uma asa em função da… (more)

Subjects/Keywords: Arrasto; Câmber; Câmber; Drag; Flape de bordo de ataque; Leading edge flap; Lift; Sustentação

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

APA (6th Edition):

Araujo Filho, M. M. d. (2008). Efeito da variação de câmber nas características aerodinâmicas de uma asa tri-dimensional. (Masters Thesis). University of São Paulo. Retrieved from http://www.teses.usp.br/teses/disponiveis/18/18148/tde-27082013-105058/ ;

Chicago Manual of Style (16th Edition):

Araujo Filho, Maurilio Messias de. “Efeito da variação de câmber nas características aerodinâmicas de uma asa tri-dimensional.” 2008. Masters Thesis, University of São Paulo. Accessed January 24, 2021. http://www.teses.usp.br/teses/disponiveis/18/18148/tde-27082013-105058/ ;.

MLA Handbook (7th Edition):

Araujo Filho, Maurilio Messias de. “Efeito da variação de câmber nas características aerodinâmicas de uma asa tri-dimensional.” 2008. Web. 24 Jan 2021.

Vancouver:

Araujo Filho MMd. Efeito da variação de câmber nas características aerodinâmicas de uma asa tri-dimensional. [Internet] [Masters thesis]. University of São Paulo; 2008. [cited 2021 Jan 24]. Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-27082013-105058/ ;.

Council of Science Editors:

Araujo Filho MMd. Efeito da variação de câmber nas características aerodinâmicas de uma asa tri-dimensional. [Masters Thesis]. University of São Paulo; 2008. Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-27082013-105058/ ;


Penn State University

16. Bhatnagar, Unmukt Rajeev. FORMULA 1 RACE CAR PERFORMANCE IMPROVEMENT BY OPTIMIZATION OF THE AERODYNAMIC RELATIONSHIP BETWEEN THE FRONT AND REAR WINGS.

Degree: 2014, Penn State University

 The sport of Formula 1 (F1) has been a proving ground for race fanatics and engineers for more than half a century. With every driver… (more)

Subjects/Keywords: Formula 1; Aerodynamics; Optimization; Lift Coefficient; Drag Coefficient; Lap Simulation; Genetic Algorithms

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

APA (6th Edition):

Bhatnagar, U. R. (2014). FORMULA 1 RACE CAR PERFORMANCE IMPROVEMENT BY OPTIMIZATION OF THE AERODYNAMIC RELATIONSHIP BETWEEN THE FRONT AND REAR WINGS. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/23699

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):

Bhatnagar, Unmukt Rajeev. “FORMULA 1 RACE CAR PERFORMANCE IMPROVEMENT BY OPTIMIZATION OF THE AERODYNAMIC RELATIONSHIP BETWEEN THE FRONT AND REAR WINGS.” 2014. Thesis, Penn State University. Accessed January 24, 2021. https://submit-etda.libraries.psu.edu/catalog/23699.

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

MLA Handbook (7th Edition):

Bhatnagar, Unmukt Rajeev. “FORMULA 1 RACE CAR PERFORMANCE IMPROVEMENT BY OPTIMIZATION OF THE AERODYNAMIC RELATIONSHIP BETWEEN THE FRONT AND REAR WINGS.” 2014. Web. 24 Jan 2021.

Vancouver:

Bhatnagar UR. FORMULA 1 RACE CAR PERFORMANCE IMPROVEMENT BY OPTIMIZATION OF THE AERODYNAMIC RELATIONSHIP BETWEEN THE FRONT AND REAR WINGS. [Internet] [Thesis]. Penn State University; 2014. [cited 2021 Jan 24]. Available from: https://submit-etda.libraries.psu.edu/catalog/23699.

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

Council of Science Editors:

Bhatnagar UR. FORMULA 1 RACE CAR PERFORMANCE IMPROVEMENT BY OPTIMIZATION OF THE AERODYNAMIC RELATIONSHIP BETWEEN THE FRONT AND REAR WINGS. [Thesis]. Penn State University; 2014. Available from: https://submit-etda.libraries.psu.edu/catalog/23699

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


Robert Gordon University

17. Iyalla, Ibiyekariwaripiribo. Computational fluid dynamics modelling of pipeline on-bottom stability.

Degree: PhD, 2017, Robert Gordon University

 Subsea pipelines are subjected to wave and steady current loads which cause pipeline stability problems. Current knowledge and understanding on the pipeline on-bottom stability is… (more)

Subjects/Keywords: 620; Drag; Embedment; Hydrodynamic force; Lateral resistance; Lift; Passive resistance; Pipeline; Pressure coefficient; Scour; Stability

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

APA (6th Edition):

Iyalla, I. (2017). Computational fluid dynamics modelling of pipeline on-bottom stability. (Doctoral Dissertation). Robert Gordon University. Retrieved from http://hdl.handle.net/10059/2721

Chicago Manual of Style (16th Edition):

Iyalla, Ibiyekariwaripiribo. “Computational fluid dynamics modelling of pipeline on-bottom stability.” 2017. Doctoral Dissertation, Robert Gordon University. Accessed January 24, 2021. http://hdl.handle.net/10059/2721.

MLA Handbook (7th Edition):

Iyalla, Ibiyekariwaripiribo. “Computational fluid dynamics modelling of pipeline on-bottom stability.” 2017. Web. 24 Jan 2021.

Vancouver:

Iyalla I. Computational fluid dynamics modelling of pipeline on-bottom stability. [Internet] [Doctoral dissertation]. Robert Gordon University; 2017. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/10059/2721.

Council of Science Editors:

Iyalla I. Computational fluid dynamics modelling of pipeline on-bottom stability. [Doctoral Dissertation]. Robert Gordon University; 2017. Available from: http://hdl.handle.net/10059/2721


Brno University of Technology

18. Martínek, Tomáš. Aerodynamická řešení podlah závodních vozů: Aerodynamics of race car underbodies.

Degree: 2019, Brno University of Technology

 The aim of this bachelor thesis is clarifying principle of downforce, which is originating by ground effect. The thesis consists of theoretic description of this… (more)

Subjects/Keywords: aerodynamika vozidel; přísavný efekt; vztlak; přítlak; odpor; automotive aerodynamics; ground effect; lift; downforce; drag

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

APA (6th Edition):

Martínek, T. (2019). Aerodynamická řešení podlah závodních vozů: Aerodynamics of race car underbodies. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/62306

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):

Martínek, Tomáš. “Aerodynamická řešení podlah závodních vozů: Aerodynamics of race car underbodies.” 2019. Thesis, Brno University of Technology. Accessed January 24, 2021. http://hdl.handle.net/11012/62306.

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

MLA Handbook (7th Edition):

Martínek, Tomáš. “Aerodynamická řešení podlah závodních vozů: Aerodynamics of race car underbodies.” 2019. Web. 24 Jan 2021.

Vancouver:

Martínek T. Aerodynamická řešení podlah závodních vozů: Aerodynamics of race car underbodies. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/11012/62306.

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

Council of Science Editors:

Martínek T. Aerodynamická řešení podlah závodních vozů: Aerodynamics of race car underbodies. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/62306

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


Brno University of Technology

19. Martinek, Tomáš. Aerodynamická řešení podlah závodních vozů: Aerodynamics of race car underbodies.

Degree: 2016, Brno University of Technology

 The aim of this bachelor thesis is clarifying principle of downforce, which is originating by ground effect. The thesis consists of theoretic description of this… (more)

Subjects/Keywords: aerodynamika vozidel; přísavný efekt; vztlak; přítlak; odpor; automotive aerodynamics; ground effect; lift; downforce; drag

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

APA (6th Edition):

Martinek, T. (2016). Aerodynamická řešení podlah závodních vozů: Aerodynamics of race car underbodies. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/60260

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):

Martinek, Tomáš. “Aerodynamická řešení podlah závodních vozů: Aerodynamics of race car underbodies.” 2016. Thesis, Brno University of Technology. Accessed January 24, 2021. http://hdl.handle.net/11012/60260.

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

MLA Handbook (7th Edition):

Martinek, Tomáš. “Aerodynamická řešení podlah závodních vozů: Aerodynamics of race car underbodies.” 2016. Web. 24 Jan 2021.

Vancouver:

Martinek T. Aerodynamická řešení podlah závodních vozů: Aerodynamics of race car underbodies. [Internet] [Thesis]. Brno University of Technology; 2016. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/11012/60260.

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

Council of Science Editors:

Martinek T. Aerodynamická řešení podlah závodních vozů: Aerodynamics of race car underbodies. [Thesis]. Brno University of Technology; 2016. Available from: http://hdl.handle.net/11012/60260

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


Brno University of Technology

20. Kazda, Adam. Vliv výrobních nepřesností na vznik přídavných momentů na kormidle jachty: Manufacturing inaccuracies influence on an appearence of the additional moment on a sailboat rudder.

Degree: 2019, Brno University of Technology

 This Master’s thesis is dedicated to a generation of an additional torque, which can occur due to the inaccuracy of the manufacturing. This issue is… (more)

Subjects/Keywords: vztlaková síla; odporová síla; jachta; kormidlo; CFD modelování; lift; drag; yacht; rudder; CFD modeling

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

APA (6th Edition):

Kazda, A. (2019). Vliv výrobních nepřesností na vznik přídavných momentů na kormidle jachty: Manufacturing inaccuracies influence on an appearence of the additional moment on a sailboat rudder. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/60785

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):

Kazda, Adam. “Vliv výrobních nepřesností na vznik přídavných momentů na kormidle jachty: Manufacturing inaccuracies influence on an appearence of the additional moment on a sailboat rudder.” 2019. Thesis, Brno University of Technology. Accessed January 24, 2021. http://hdl.handle.net/11012/60785.

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

MLA Handbook (7th Edition):

Kazda, Adam. “Vliv výrobních nepřesností na vznik přídavných momentů na kormidle jachty: Manufacturing inaccuracies influence on an appearence of the additional moment on a sailboat rudder.” 2019. Web. 24 Jan 2021.

Vancouver:

Kazda A. Vliv výrobních nepřesností na vznik přídavných momentů na kormidle jachty: Manufacturing inaccuracies influence on an appearence of the additional moment on a sailboat rudder. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/11012/60785.

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

Council of Science Editors:

Kazda A. Vliv výrobních nepřesností na vznik přídavných momentů na kormidle jachty: Manufacturing inaccuracies influence on an appearence of the additional moment on a sailboat rudder. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/60785

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


Cal Poly

21. Bergman, William H. A Study of the Standard Cirrus Wing Lift Distribution Versus Bell Shaped Lift Distribution.

Degree: MS, Aerospace Engineering, 2020, Cal Poly

  This thesis discusses a comparison of the differences in aerodynamic performance of wings designed with elliptical and bell-shaped lift distributions. The method uses a… (more)

Subjects/Keywords: lift distribution; bell-shaped; induced drag; skin friction; Aerodynamics and Fluid Mechanics; Aeronautical Vehicles

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

APA (6th Edition):

Bergman, W. H. (2020). A Study of the Standard Cirrus Wing Lift Distribution Versus Bell Shaped Lift Distribution. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/2178 ; 10.15368/theses.2020.59

Chicago Manual of Style (16th Edition):

Bergman, William H. “A Study of the Standard Cirrus Wing Lift Distribution Versus Bell Shaped Lift Distribution.” 2020. Masters Thesis, Cal Poly. Accessed January 24, 2021. https://digitalcommons.calpoly.edu/theses/2178 ; 10.15368/theses.2020.59.

MLA Handbook (7th Edition):

Bergman, William H. “A Study of the Standard Cirrus Wing Lift Distribution Versus Bell Shaped Lift Distribution.” 2020. Web. 24 Jan 2021.

Vancouver:

Bergman WH. A Study of the Standard Cirrus Wing Lift Distribution Versus Bell Shaped Lift Distribution. [Internet] [Masters thesis]. Cal Poly; 2020. [cited 2021 Jan 24]. Available from: https://digitalcommons.calpoly.edu/theses/2178 ; 10.15368/theses.2020.59.

Council of Science Editors:

Bergman WH. A Study of the Standard Cirrus Wing Lift Distribution Versus Bell Shaped Lift Distribution. [Masters Thesis]. Cal Poly; 2020. Available from: https://digitalcommons.calpoly.edu/theses/2178 ; 10.15368/theses.2020.59


NSYSU

22. Tsuo, Cheng-Wen. Scarcity Product, Perceived Risk and Expected Product Price Impact on Purchase Intentionï¼Social Identification Needs and Conspicuous Consumption as the Moderator.

Degree: Master, Institute Of Marketing Communication, 2018, NSYSU

 Regarding to the hunger marketing is increasingly appearing in the market, the effect of scarcity product has become increasingly important for both consumers and businesses.… (more)

Subjects/Keywords: scarcity product; scarcity due to supply; scarcity due to demand; expected product price; perceived risk; social identity; conspicuous consumption

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

APA (6th Edition):

Tsuo, C. (2018). Scarcity Product, Perceived Risk and Expected Product Price Impact on Purchase Intentionï¼Social Identification Needs and Conspicuous Consumption as the Moderator. (Thesis). NSYSU. Retrieved from http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0725118-160533

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):

Tsuo, Cheng-Wen. “Scarcity Product, Perceived Risk and Expected Product Price Impact on Purchase Intentionï¼Social Identification Needs and Conspicuous Consumption as the Moderator.” 2018. Thesis, NSYSU. Accessed January 24, 2021. http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0725118-160533.

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

MLA Handbook (7th Edition):

Tsuo, Cheng-Wen. “Scarcity Product, Perceived Risk and Expected Product Price Impact on Purchase Intentionï¼Social Identification Needs and Conspicuous Consumption as the Moderator.” 2018. Web. 24 Jan 2021.

Vancouver:

Tsuo C. Scarcity Product, Perceived Risk and Expected Product Price Impact on Purchase Intentionï¼Social Identification Needs and Conspicuous Consumption as the Moderator. [Internet] [Thesis]. NSYSU; 2018. [cited 2021 Jan 24]. Available from: http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0725118-160533.

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

Council of Science Editors:

Tsuo C. Scarcity Product, Perceived Risk and Expected Product Price Impact on Purchase Intentionï¼Social Identification Needs and Conspicuous Consumption as the Moderator. [Thesis]. NSYSU; 2018. Available from: http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0725118-160533

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


Technical University of Lisbon

23. Barros, David Alexandre Lampreia. Analise e caracterização do ruído ambiente urbano. Cidade de Lisboa - Bairro habitacional.

Degree: 2011, Technical University of Lisbon

Mestrado em Engenharia do Ambiente - Instituto Superior de Agronomia

The work of this dissertation focuses essentially on matters related to the areas of environmental… (more)

Subjects/Keywords: noise; environmental acoustics; urban noise; disconfort due to noise

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

APA (6th Edition):

Barros, D. A. L. (2011). Analise e caracterização do ruído ambiente urbano. Cidade de Lisboa - Bairro habitacional. (Thesis). Technical University of Lisbon. Retrieved from http://www.rcaap.pt/detail.jsp?id=oai:www.repository.utl.pt:10400.5/4030

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):

Barros, David Alexandre Lampreia. “Analise e caracterização do ruído ambiente urbano. Cidade de Lisboa - Bairro habitacional.” 2011. Thesis, Technical University of Lisbon. Accessed January 24, 2021. http://www.rcaap.pt/detail.jsp?id=oai:www.repository.utl.pt:10400.5/4030.

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

MLA Handbook (7th Edition):

Barros, David Alexandre Lampreia. “Analise e caracterização do ruído ambiente urbano. Cidade de Lisboa - Bairro habitacional.” 2011. Web. 24 Jan 2021.

Vancouver:

Barros DAL. Analise e caracterização do ruído ambiente urbano. Cidade de Lisboa - Bairro habitacional. [Internet] [Thesis]. Technical University of Lisbon; 2011. [cited 2021 Jan 24]. Available from: http://www.rcaap.pt/detail.jsp?id=oai:www.repository.utl.pt:10400.5/4030.

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

Council of Science Editors:

Barros DAL. Analise e caracterização do ruído ambiente urbano. Cidade de Lisboa - Bairro habitacional. [Thesis]. Technical University of Lisbon; 2011. Available from: http://www.rcaap.pt/detail.jsp?id=oai:www.repository.utl.pt:10400.5/4030

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


University of Michigan

24. Amur Varadarajan, Prasanna. Noise Transmission along Shock Waves.

Degree: PhD, Aerospace Engineering, 2011, University of Michigan

 Shocks at the inlet of scramjet engines are subject to perturbations from their interaction with turbulent boundary layer. DNS results for this interaction indicate the… (more)

Subjects/Keywords: Perturbations Along the Shocks Due to Vortex Interaction; Aerospace Engineering; Engineering

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

APA (6th Edition):

Amur Varadarajan, P. (2011). Noise Transmission along Shock Waves. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/89612

Chicago Manual of Style (16th Edition):

Amur Varadarajan, Prasanna. “Noise Transmission along Shock Waves.” 2011. Doctoral Dissertation, University of Michigan. Accessed January 24, 2021. http://hdl.handle.net/2027.42/89612.

MLA Handbook (7th Edition):

Amur Varadarajan, Prasanna. “Noise Transmission along Shock Waves.” 2011. Web. 24 Jan 2021.

Vancouver:

Amur Varadarajan P. Noise Transmission along Shock Waves. [Internet] [Doctoral dissertation]. University of Michigan; 2011. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/2027.42/89612.

Council of Science Editors:

Amur Varadarajan P. Noise Transmission along Shock Waves. [Doctoral Dissertation]. University of Michigan; 2011. Available from: http://hdl.handle.net/2027.42/89612


North Carolina State University

25. Shipley, Edward Nicholas Jr. Static Aeroelasticity Considerations in Aerodynamic Adaptation of Wings for Low Drag.

Degree: MS, Aerospace Engineering, 2006, North Carolina State University

 This thesis presents a methodology to calculate the flap angles necessary to reproduce a desired lift distribution for an elastic wing with multiple trailing-edge flaps.… (more)

Subjects/Keywords: adaptive wing; elliptic lift; profile drag; induced drag; aerodynamics; aeroelasticity

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

APA (6th Edition):

Shipley, E. N. J. (2006). Static Aeroelasticity Considerations in Aerodynamic Adaptation of Wings for Low Drag. (Thesis). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/1118

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):

Shipley, Edward Nicholas Jr. “Static Aeroelasticity Considerations in Aerodynamic Adaptation of Wings for Low Drag.” 2006. Thesis, North Carolina State University. Accessed January 24, 2021. http://www.lib.ncsu.edu/resolver/1840.16/1118.

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

MLA Handbook (7th Edition):

Shipley, Edward Nicholas Jr. “Static Aeroelasticity Considerations in Aerodynamic Adaptation of Wings for Low Drag.” 2006. Web. 24 Jan 2021.

Vancouver:

Shipley ENJ. Static Aeroelasticity Considerations in Aerodynamic Adaptation of Wings for Low Drag. [Internet] [Thesis]. North Carolina State University; 2006. [cited 2021 Jan 24]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/1118.

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

Council of Science Editors:

Shipley ENJ. Static Aeroelasticity Considerations in Aerodynamic Adaptation of Wings for Low Drag. [Thesis]. North Carolina State University; 2006. Available from: http://www.lib.ncsu.edu/resolver/1840.16/1118

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

26. Fernanda Alves Ribeiro. Análise aerodinâmica de perfis de asa para aeronaves experimentais tipo jn-1.

Degree: 2011, Universidade Federal do Rio Grande do Norte

A importância na escolha do perfil de asa de uma aeronave é função de sua relevância no seu desempenho; influenciando desde os custos de deslocamento… (more)

Subjects/Keywords: Arodinâmica; Perfil de asa; Coeficiente de arrasto; Coeficiente de sustentação; ENGENHARIA MECANICA; Aerodynamics; Wing profile; Drag coefficient; Lift coefficient

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

APA (6th Edition):

Ribeiro, F. A. (2011). Análise aerodinâmica de perfis de asa para aeronaves experimentais tipo jn-1. (Thesis). Universidade Federal do Rio Grande do Norte. Retrieved from http://bdtd.bczm.ufrn.br/tedesimplificado//tde_busca/arquivo.php?codArquivo=4769

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):

Ribeiro, Fernanda Alves. “Análise aerodinâmica de perfis de asa para aeronaves experimentais tipo jn-1.” 2011. Thesis, Universidade Federal do Rio Grande do Norte. Accessed January 24, 2021. http://bdtd.bczm.ufrn.br/tedesimplificado//tde_busca/arquivo.php?codArquivo=4769.

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

MLA Handbook (7th Edition):

Ribeiro, Fernanda Alves. “Análise aerodinâmica de perfis de asa para aeronaves experimentais tipo jn-1.” 2011. Web. 24 Jan 2021.

Vancouver:

Ribeiro FA. Análise aerodinâmica de perfis de asa para aeronaves experimentais tipo jn-1. [Internet] [Thesis]. Universidade Federal do Rio Grande do Norte; 2011. [cited 2021 Jan 24]. Available from: http://bdtd.bczm.ufrn.br/tedesimplificado//tde_busca/arquivo.php?codArquivo=4769.

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

Council of Science Editors:

Ribeiro FA. Análise aerodinâmica de perfis de asa para aeronaves experimentais tipo jn-1. [Thesis]. Universidade Federal do Rio Grande do Norte; 2011. Available from: http://bdtd.bczm.ufrn.br/tedesimplificado//tde_busca/arquivo.php?codArquivo=4769

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


Universidade do Rio Grande do Norte

27. Ribeiro, Fernanda Alves. Análise aerodinâmica de perfis de asa para aeronaves experimentais tipo jn-1 .

Degree: 2011, Universidade do Rio Grande do Norte

 The great importance in selecting the profile of an aircraft wing concerns the fact that its relevance in the performance thereof; influencing this displacement costs… (more)

Subjects/Keywords: Arodinâmica; Perfil de asa; Coeficiente de arrasto; Coeficiente de sustentação; Aerodynamics; Wing profile; Drag coefficient; Lift coefficient

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

APA (6th Edition):

Ribeiro, F. A. (2011). Análise aerodinâmica de perfis de asa para aeronaves experimentais tipo jn-1 . (Masters Thesis). Universidade do Rio Grande do Norte. Retrieved from http://repositorio.ufrn.br/handle/123456789/15657

Chicago Manual of Style (16th Edition):

Ribeiro, Fernanda Alves. “Análise aerodinâmica de perfis de asa para aeronaves experimentais tipo jn-1 .” 2011. Masters Thesis, Universidade do Rio Grande do Norte. Accessed January 24, 2021. http://repositorio.ufrn.br/handle/123456789/15657.

MLA Handbook (7th Edition):

Ribeiro, Fernanda Alves. “Análise aerodinâmica de perfis de asa para aeronaves experimentais tipo jn-1 .” 2011. Web. 24 Jan 2021.

Vancouver:

Ribeiro FA. Análise aerodinâmica de perfis de asa para aeronaves experimentais tipo jn-1 . [Internet] [Masters thesis]. Universidade do Rio Grande do Norte; 2011. [cited 2021 Jan 24]. Available from: http://repositorio.ufrn.br/handle/123456789/15657.

Council of Science Editors:

Ribeiro FA. Análise aerodinâmica de perfis de asa para aeronaves experimentais tipo jn-1 . [Masters Thesis]. Universidade do Rio Grande do Norte; 2011. Available from: http://repositorio.ufrn.br/handle/123456789/15657


Universidade do Rio Grande do Norte

28. Ribeiro, Fernanda Alves. Análise aerodinâmica de perfis de asa para aeronaves experimentais tipo jn-1 .

Degree: 2011, Universidade do Rio Grande do Norte

 The great importance in selecting the profile of an aircraft wing concerns the fact that its relevance in the performance thereof; influencing this displacement costs… (more)

Subjects/Keywords: Arodinâmica; Perfil de asa; Coeficiente de arrasto; Coeficiente de sustentação; Aerodynamics; Wing profile; Drag coefficient; Lift coefficient

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Ribeiro, F. A. (2011). Análise aerodinâmica de perfis de asa para aeronaves experimentais tipo jn-1 . (Thesis). Universidade do Rio Grande do Norte. Retrieved from http://repositorio.ufrn.br/handle/123456789/15657

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):

Ribeiro, Fernanda Alves. “Análise aerodinâmica de perfis de asa para aeronaves experimentais tipo jn-1 .” 2011. Thesis, Universidade do Rio Grande do Norte. Accessed January 24, 2021. http://repositorio.ufrn.br/handle/123456789/15657.

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

MLA Handbook (7th Edition):

Ribeiro, Fernanda Alves. “Análise aerodinâmica de perfis de asa para aeronaves experimentais tipo jn-1 .” 2011. Web. 24 Jan 2021.

Vancouver:

Ribeiro FA. Análise aerodinâmica de perfis de asa para aeronaves experimentais tipo jn-1 . [Internet] [Thesis]. Universidade do Rio Grande do Norte; 2011. [cited 2021 Jan 24]. Available from: http://repositorio.ufrn.br/handle/123456789/15657.

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

Council of Science Editors:

Ribeiro FA. Análise aerodinâmica de perfis de asa para aeronaves experimentais tipo jn-1 . [Thesis]. Universidade do Rio Grande do Norte; 2011. Available from: http://repositorio.ufrn.br/handle/123456789/15657

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


Brigham Young University

29. Parekh, M. B. Determination of Drag and Lift Coefficients for a Spinning Baseball.

Degree: MS, 1972, Brigham Young University

  Few experiments have been carried out in the past to deter mine the effect of the lift and the drag forces on the trajectory… (more)

Subjects/Keywords: Drag (Aerodynamics); Lift (Aerodynamics); Projectiles; Mechanical Engineering

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

APA (6th Edition):

Parekh, M. B. (1972). Determination of Drag and Lift Coefficients for a Spinning Baseball. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=8163&context=etd

Chicago Manual of Style (16th Edition):

Parekh, M B. “Determination of Drag and Lift Coefficients for a Spinning Baseball.” 1972. Masters Thesis, Brigham Young University. Accessed January 24, 2021. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=8163&context=etd.

MLA Handbook (7th Edition):

Parekh, M B. “Determination of Drag and Lift Coefficients for a Spinning Baseball.” 1972. Web. 24 Jan 2021.

Vancouver:

Parekh MB. Determination of Drag and Lift Coefficients for a Spinning Baseball. [Internet] [Masters thesis]. Brigham Young University; 1972. [cited 2021 Jan 24]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=8163&context=etd.

Council of Science Editors:

Parekh MB. Determination of Drag and Lift Coefficients for a Spinning Baseball. [Masters Thesis]. Brigham Young University; 1972. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=8163&context=etd


Université de Lorraine

30. Ouchene, Rafik. Dispersion de particules non-sphériques en écoulement turbulent : Dispersion of non spherical particles in a turbulent flow.

Degree: Docteur es, Mécanique et énergétique, 2015, Université de Lorraine

Ce travail de thèse fait partie intégrante de l’ANR PLAYER (début janvier 2012), projet visant à étendre les simulations d'écoulements gaz-particules à des particules non-sphériques… (more)

Subjects/Keywords: Force hydrodynamique; Traînée; Portance; Couple; Particules ellipsoïdales; DNS; Turbulence; Dispersion; Hydrodynamic forces; Drag; Lift; Torque; Ellipsoidal particles; DNS; Turbulence; Dispersion; 532.5

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

APA (6th Edition):

Ouchene, R. (2015). Dispersion de particules non-sphériques en écoulement turbulent : Dispersion of non spherical particles in a turbulent flow. (Doctoral Dissertation). Université de Lorraine. Retrieved from http://www.theses.fr/2015LORR0275

Chicago Manual of Style (16th Edition):

Ouchene, Rafik. “Dispersion de particules non-sphériques en écoulement turbulent : Dispersion of non spherical particles in a turbulent flow.” 2015. Doctoral Dissertation, Université de Lorraine. Accessed January 24, 2021. http://www.theses.fr/2015LORR0275.

MLA Handbook (7th Edition):

Ouchene, Rafik. “Dispersion de particules non-sphériques en écoulement turbulent : Dispersion of non spherical particles in a turbulent flow.” 2015. Web. 24 Jan 2021.

Vancouver:

Ouchene R. Dispersion de particules non-sphériques en écoulement turbulent : Dispersion of non spherical particles in a turbulent flow. [Internet] [Doctoral dissertation]. Université de Lorraine; 2015. [cited 2021 Jan 24]. Available from: http://www.theses.fr/2015LORR0275.

Council of Science Editors:

Ouchene R. Dispersion de particules non-sphériques en écoulement turbulent : Dispersion of non spherical particles in a turbulent flow. [Doctoral Dissertation]. Université de Lorraine; 2015. Available from: http://www.theses.fr/2015LORR0275

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