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You searched for subject:(Aerodynamics AND Fluid Mechanics). Showing records 1 – 30 of 572 total matches.

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Cal Poly

1. Thomason, Nicole M. Experimental Investigation of Suction Slot Geometry on a Goldschmied Propulsor.

Degree: MS, Aerospace Engineering, 2012, Cal Poly

  The Goldschmied Propulsor concept combines boundary layer suction and boundary layer ingestion to improve propulsive efficiency and reduce drag on an axisymmetric body. This… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics

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APA (6th Edition):

Thomason, N. M. (2012). Experimental Investigation of Suction Slot Geometry on a Goldschmied Propulsor. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/689 ; 10.15368/theses.2012.6

Chicago Manual of Style (16th Edition):

Thomason, Nicole M. “Experimental Investigation of Suction Slot Geometry on a Goldschmied Propulsor.” 2012. Masters Thesis, Cal Poly. Accessed February 23, 2020. https://digitalcommons.calpoly.edu/theses/689 ; 10.15368/theses.2012.6.

MLA Handbook (7th Edition):

Thomason, Nicole M. “Experimental Investigation of Suction Slot Geometry on a Goldschmied Propulsor.” 2012. Web. 23 Feb 2020.

Vancouver:

Thomason NM. Experimental Investigation of Suction Slot Geometry on a Goldschmied Propulsor. [Internet] [Masters thesis]. Cal Poly; 2012. [cited 2020 Feb 23]. Available from: https://digitalcommons.calpoly.edu/theses/689 ; 10.15368/theses.2012.6.

Council of Science Editors:

Thomason NM. Experimental Investigation of Suction Slot Geometry on a Goldschmied Propulsor. [Masters Thesis]. Cal Poly; 2012. Available from: https://digitalcommons.calpoly.edu/theses/689 ; 10.15368/theses.2012.6


Cal Poly

2. Erlhoff, Ethan Bruce. Distributed Forcing on a 3D Bluff Body with a Blunt Base, An Experimental Active Drag Control Approach.

Degree: MS, Aerospace Engineering, 2012, Cal Poly

  This paper seeks to explore the effects of an active drag control method known as distributed forcing on a 3D bluff body with a… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics

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APA (6th Edition):

Erlhoff, E. B. (2012). Distributed Forcing on a 3D Bluff Body with a Blunt Base, An Experimental Active Drag Control Approach. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/879 ; 10.15368/theses.2012.201

Chicago Manual of Style (16th Edition):

Erlhoff, Ethan Bruce. “Distributed Forcing on a 3D Bluff Body with a Blunt Base, An Experimental Active Drag Control Approach.” 2012. Masters Thesis, Cal Poly. Accessed February 23, 2020. https://digitalcommons.calpoly.edu/theses/879 ; 10.15368/theses.2012.201.

MLA Handbook (7th Edition):

Erlhoff, Ethan Bruce. “Distributed Forcing on a 3D Bluff Body with a Blunt Base, An Experimental Active Drag Control Approach.” 2012. Web. 23 Feb 2020.

Vancouver:

Erlhoff EB. Distributed Forcing on a 3D Bluff Body with a Blunt Base, An Experimental Active Drag Control Approach. [Internet] [Masters thesis]. Cal Poly; 2012. [cited 2020 Feb 23]. Available from: https://digitalcommons.calpoly.edu/theses/879 ; 10.15368/theses.2012.201.

Council of Science Editors:

Erlhoff EB. Distributed Forcing on a 3D Bluff Body with a Blunt Base, An Experimental Active Drag Control Approach. [Masters Thesis]. Cal Poly; 2012. Available from: https://digitalcommons.calpoly.edu/theses/879 ; 10.15368/theses.2012.201


Embry-Riddle Aeronautical University

3. Paul, Leander. Study of Hybrid Magneto-Active Propellant Management Device for Slosh Damping.

Degree: MSin Aerospace Engineering, Graduate Studies, 2016, Embry-Riddle Aeronautical University

  Sloshing of liquid upon the application of an external force is a natural phenomenon as the free surface is allowed to move without any… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics

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APA (6th Edition):

Paul, L. (2016). Study of Hybrid Magneto-Active Propellant Management Device for Slosh Damping. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/230

Chicago Manual of Style (16th Edition):

Paul, Leander. “Study of Hybrid Magneto-Active Propellant Management Device for Slosh Damping.” 2016. Masters Thesis, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/230.

MLA Handbook (7th Edition):

Paul, Leander. “Study of Hybrid Magneto-Active Propellant Management Device for Slosh Damping.” 2016. Web. 23 Feb 2020.

Vancouver:

Paul L. Study of Hybrid Magneto-Active Propellant Management Device for Slosh Damping. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2016. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/230.

Council of Science Editors:

Paul L. Study of Hybrid Magneto-Active Propellant Management Device for Slosh Damping. [Masters Thesis]. Embry-Riddle Aeronautical University; 2016. Available from: https://commons.erau.edu/edt/230


Embry-Riddle Aeronautical University

4. Lowe, Jarrett E. Fluidic Jet Turbulence Generators for Deflagration to Detonation Transition in Pulsed Detonation Combustors.

Degree: MSin Aerospace Engineering, Graduate Studies, 2016, Embry-Riddle Aeronautical University

  The goal of this study is to establish the dominant flow structure required to effectively accelerate the turbulent deflagration flame front to detonation velocity… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics

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APA (6th Edition):

Lowe, J. E. (2016). Fluidic Jet Turbulence Generators for Deflagration to Detonation Transition in Pulsed Detonation Combustors. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/224

Chicago Manual of Style (16th Edition):

Lowe, Jarrett E. “Fluidic Jet Turbulence Generators for Deflagration to Detonation Transition in Pulsed Detonation Combustors.” 2016. Masters Thesis, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/224.

MLA Handbook (7th Edition):

Lowe, Jarrett E. “Fluidic Jet Turbulence Generators for Deflagration to Detonation Transition in Pulsed Detonation Combustors.” 2016. Web. 23 Feb 2020.

Vancouver:

Lowe JE. Fluidic Jet Turbulence Generators for Deflagration to Detonation Transition in Pulsed Detonation Combustors. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2016. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/224.

Council of Science Editors:

Lowe JE. Fluidic Jet Turbulence Generators for Deflagration to Detonation Transition in Pulsed Detonation Combustors. [Masters Thesis]. Embry-Riddle Aeronautical University; 2016. Available from: https://commons.erau.edu/edt/224


Embry-Riddle Aeronautical University

5. Vijayanarayanan, Arjun. Development of a Higher-Order Navier-Stokes Solver for Transient Compressible Flows.

Degree: MSin Aerospace Engineering, Aerospace Engineering, 2011, Embry-Riddle Aeronautical University

  A higher‐order density based navier‐stokes solver was developed for 2‐Dimensional flows using the finite volume approach. The Van leer flux‐splitting technique was used to… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics

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APA (6th Edition):

Vijayanarayanan, A. (2011). Development of a Higher-Order Navier-Stokes Solver for Transient Compressible Flows. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/256

Chicago Manual of Style (16th Edition):

Vijayanarayanan, Arjun. “Development of a Higher-Order Navier-Stokes Solver for Transient Compressible Flows.” 2011. Masters Thesis, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/256.

MLA Handbook (7th Edition):

Vijayanarayanan, Arjun. “Development of a Higher-Order Navier-Stokes Solver for Transient Compressible Flows.” 2011. Web. 23 Feb 2020.

Vancouver:

Vijayanarayanan A. Development of a Higher-Order Navier-Stokes Solver for Transient Compressible Flows. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2011. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/256.

Council of Science Editors:

Vijayanarayanan A. Development of a Higher-Order Navier-Stokes Solver for Transient Compressible Flows. [Masters Thesis]. Embry-Riddle Aeronautical University; 2011. Available from: https://commons.erau.edu/edt/256


Embry-Riddle Aeronautical University

6. Xavier, Sathish. Numerical Analysis of Gun Barrel Pressure Blast Using Dynamic Mesh Adaption.

Degree: MSin Aerospace Engineering, Aerospace Engineering, 2011, Embry-Riddle Aeronautical University

  A Computational Fluid Dynamics (CFD) method has been applied to simulate the pressure blast of the projectile which is launched from a barrel and… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics

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APA (6th Edition):

Xavier, S. (2011). Numerical Analysis of Gun Barrel Pressure Blast Using Dynamic Mesh Adaption. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/258

Chicago Manual of Style (16th Edition):

Xavier, Sathish. “Numerical Analysis of Gun Barrel Pressure Blast Using Dynamic Mesh Adaption.” 2011. Masters Thesis, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/258.

MLA Handbook (7th Edition):

Xavier, Sathish. “Numerical Analysis of Gun Barrel Pressure Blast Using Dynamic Mesh Adaption.” 2011. Web. 23 Feb 2020.

Vancouver:

Xavier S. Numerical Analysis of Gun Barrel Pressure Blast Using Dynamic Mesh Adaption. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2011. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/258.

Council of Science Editors:

Xavier S. Numerical Analysis of Gun Barrel Pressure Blast Using Dynamic Mesh Adaption. [Masters Thesis]. Embry-Riddle Aeronautical University; 2011. Available from: https://commons.erau.edu/edt/258


Embry-Riddle Aeronautical University

7. Rane, Jitesh. Similarity Analysis of a Swirling Counter-Flow.

Degree: MSin Aerospace Engineering, Graduate Studies, 2015, Embry-Riddle Aeronautical University

  Swirling counter-flows are used in numerous engineering applications, like combustion, heat exchangers, cyclonic separation and mixing, etc. These swirling counter-flows produce complex flow fields.… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics

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APA (6th Edition):

Rane, J. (2015). Similarity Analysis of a Swirling Counter-Flow. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/235

Chicago Manual of Style (16th Edition):

Rane, Jitesh. “Similarity Analysis of a Swirling Counter-Flow.” 2015. Masters Thesis, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/235.

MLA Handbook (7th Edition):

Rane, Jitesh. “Similarity Analysis of a Swirling Counter-Flow.” 2015. Web. 23 Feb 2020.

Vancouver:

Rane J. Similarity Analysis of a Swirling Counter-Flow. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2015. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/235.

Council of Science Editors:

Rane J. Similarity Analysis of a Swirling Counter-Flow. [Masters Thesis]. Embry-Riddle Aeronautical University; 2015. Available from: https://commons.erau.edu/edt/235


Embry-Riddle Aeronautical University

8. Granizo, Juan F. Effect of Slot Span on Wing Performance.

Degree: MSin Aerospace Engineering, Graduate Studies, 2016, Embry-Riddle Aeronautical University

  This report presents new numerically-derived correlations to estimate the aerodynamic properties of a three-dimensional wing that features a partial to full span fixed slot.… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics

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APA (6th Edition):

Granizo, J. F. (2016). Effect of Slot Span on Wing Performance. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/301

Chicago Manual of Style (16th Edition):

Granizo, Juan F. “Effect of Slot Span on Wing Performance.” 2016. Masters Thesis, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/301.

MLA Handbook (7th Edition):

Granizo, Juan F. “Effect of Slot Span on Wing Performance.” 2016. Web. 23 Feb 2020.

Vancouver:

Granizo JF. Effect of Slot Span on Wing Performance. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2016. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/301.

Council of Science Editors:

Granizo JF. Effect of Slot Span on Wing Performance. [Masters Thesis]. Embry-Riddle Aeronautical University; 2016. Available from: https://commons.erau.edu/edt/301


Embry-Riddle Aeronautical University

9. Hayden, Joseph. Effect of Flow-Acoustic Resonant Interactions on Aerodynamic Response of Transitional Airfoils.

Degree: MSin Aerospace Engineering, Graduate Studies, 2016, Embry-Riddle Aeronautical University

  A high-accuracy numerical study is conducted to examine the impact of flow-acoustic resonant interactions on the aerodynamic response of symmetric and cambered airfoils in… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics

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APA (6th Edition):

Hayden, J. (2016). Effect of Flow-Acoustic Resonant Interactions on Aerodynamic Response of Transitional Airfoils. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/302

Chicago Manual of Style (16th Edition):

Hayden, Joseph. “Effect of Flow-Acoustic Resonant Interactions on Aerodynamic Response of Transitional Airfoils.” 2016. Masters Thesis, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/302.

MLA Handbook (7th Edition):

Hayden, Joseph. “Effect of Flow-Acoustic Resonant Interactions on Aerodynamic Response of Transitional Airfoils.” 2016. Web. 23 Feb 2020.

Vancouver:

Hayden J. Effect of Flow-Acoustic Resonant Interactions on Aerodynamic Response of Transitional Airfoils. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2016. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/302.

Council of Science Editors:

Hayden J. Effect of Flow-Acoustic Resonant Interactions on Aerodynamic Response of Transitional Airfoils. [Masters Thesis]. Embry-Riddle Aeronautical University; 2016. Available from: https://commons.erau.edu/edt/302


Embry-Riddle Aeronautical University

10. Rozendaal, Alexander V. A Computer Program for the Coupled Implementation of Meanline and Throughflow Methods to Simplify the Aerodynamic Design of Multistage Axial Compressors.

Degree: MSin Aerospace Engineering, Graduate Studies, 2016, Embry-Riddle Aeronautical University

  A computer program capable of simplifying the preliminary aerodynamic design process of multistage axial compressors has been developed. This interactive design tool, named C-STAAC,… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics

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APA (6th Edition):

Rozendaal, A. V. (2016). A Computer Program for the Coupled Implementation of Meanline and Throughflow Methods to Simplify the Aerodynamic Design of Multistage Axial Compressors. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/313

Chicago Manual of Style (16th Edition):

Rozendaal, Alexander V. “A Computer Program for the Coupled Implementation of Meanline and Throughflow Methods to Simplify the Aerodynamic Design of Multistage Axial Compressors.” 2016. Masters Thesis, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/313.

MLA Handbook (7th Edition):

Rozendaal, Alexander V. “A Computer Program for the Coupled Implementation of Meanline and Throughflow Methods to Simplify the Aerodynamic Design of Multistage Axial Compressors.” 2016. Web. 23 Feb 2020.

Vancouver:

Rozendaal AV. A Computer Program for the Coupled Implementation of Meanline and Throughflow Methods to Simplify the Aerodynamic Design of Multistage Axial Compressors. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2016. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/313.

Council of Science Editors:

Rozendaal AV. A Computer Program for the Coupled Implementation of Meanline and Throughflow Methods to Simplify the Aerodynamic Design of Multistage Axial Compressors. [Masters Thesis]. Embry-Riddle Aeronautical University; 2016. Available from: https://commons.erau.edu/edt/313


Embry-Riddle Aeronautical University

11. Coderoni, Marco. A Computational Analysis of the Aerodynamics and Aeroacoustics of Jets with Fluid Injection.

Degree: PhD, Graduate Studies, 2018, Embry-Riddle Aeronautical University

  A detailed numerical analysis of fluidic injection as a tool to reduce noise emission is presented here. The noise reduction strategy, developed at the… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics

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APA (6th Edition):

Coderoni, M. (2018). A Computational Analysis of the Aerodynamics and Aeroacoustics of Jets with Fluid Injection. (Doctoral Dissertation). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/406

Chicago Manual of Style (16th Edition):

Coderoni, Marco. “A Computational Analysis of the Aerodynamics and Aeroacoustics of Jets with Fluid Injection.” 2018. Doctoral Dissertation, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/406.

MLA Handbook (7th Edition):

Coderoni, Marco. “A Computational Analysis of the Aerodynamics and Aeroacoustics of Jets with Fluid Injection.” 2018. Web. 23 Feb 2020.

Vancouver:

Coderoni M. A Computational Analysis of the Aerodynamics and Aeroacoustics of Jets with Fluid Injection. [Internet] [Doctoral dissertation]. Embry-Riddle Aeronautical University; 2018. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/406.

Council of Science Editors:

Coderoni M. A Computational Analysis of the Aerodynamics and Aeroacoustics of Jets with Fluid Injection. [Doctoral Dissertation]. Embry-Riddle Aeronautical University; 2018. Available from: https://commons.erau.edu/edt/406


Embry-Riddle Aeronautical University

12. Hoffman, Derek. Nonlinear Control of Underactuated and Constrained Systems.

Degree: PhD, Physical Sciences, 2018, Embry-Riddle Aeronautical University

  It is the purpose of this document to elaborate on the control of systems that are underactuated or otherwise constrained. To do so, local-… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics

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APA (6th Edition):

Hoffman, D. (2018). Nonlinear Control of Underactuated and Constrained Systems. (Doctoral Dissertation). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/383

Chicago Manual of Style (16th Edition):

Hoffman, Derek. “Nonlinear Control of Underactuated and Constrained Systems.” 2018. Doctoral Dissertation, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/383.

MLA Handbook (7th Edition):

Hoffman, Derek. “Nonlinear Control of Underactuated and Constrained Systems.” 2018. Web. 23 Feb 2020.

Vancouver:

Hoffman D. Nonlinear Control of Underactuated and Constrained Systems. [Internet] [Doctoral dissertation]. Embry-Riddle Aeronautical University; 2018. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/383.

Council of Science Editors:

Hoffman D. Nonlinear Control of Underactuated and Constrained Systems. [Doctoral Dissertation]. Embry-Riddle Aeronautical University; 2018. Available from: https://commons.erau.edu/edt/383


Embry-Riddle Aeronautical University

13. Malik, Aryslan. Experimental and Computational Analysis of a 3D Printed Wing Structure.

Degree: MSin Aerospace Engineering, Graduate Studies, 2019, Embry-Riddle Aeronautical University

  Correct prediction of aeroelastic response is a crucial part in designing flutter or divergence free aircrafts within a designated flight envelope. The aeroelastic analysis… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics

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APA (6th Edition):

Malik, A. (2019). Experimental and Computational Analysis of a 3D Printed Wing Structure. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/440

Chicago Manual of Style (16th Edition):

Malik, Aryslan. “Experimental and Computational Analysis of a 3D Printed Wing Structure.” 2019. Masters Thesis, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/440.

MLA Handbook (7th Edition):

Malik, Aryslan. “Experimental and Computational Analysis of a 3D Printed Wing Structure.” 2019. Web. 23 Feb 2020.

Vancouver:

Malik A. Experimental and Computational Analysis of a 3D Printed Wing Structure. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2019. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/440.

Council of Science Editors:

Malik A. Experimental and Computational Analysis of a 3D Printed Wing Structure. [Masters Thesis]. Embry-Riddle Aeronautical University; 2019. Available from: https://commons.erau.edu/edt/440


Embry-Riddle Aeronautical University

14. Zurita, Christian A. Guzman. Preliminary Test Predictions for Scale Ram-Air Parachute Testing.

Degree: MSin Aerospace Engineering, Graduate Studies, 2019, Embry-Riddle Aeronautical University

  The present thesis proposes a preliminary analysis to predict the aerodynamic performance for experimental tests of ram-air parachutes in a wind tunnel. A scaled… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics

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APA (6th Edition):

Zurita, C. A. G. (2019). Preliminary Test Predictions for Scale Ram-Air Parachute Testing. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/446

Chicago Manual of Style (16th Edition):

Zurita, Christian A Guzman. “Preliminary Test Predictions for Scale Ram-Air Parachute Testing.” 2019. Masters Thesis, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/446.

MLA Handbook (7th Edition):

Zurita, Christian A Guzman. “Preliminary Test Predictions for Scale Ram-Air Parachute Testing.” 2019. Web. 23 Feb 2020.

Vancouver:

Zurita CAG. Preliminary Test Predictions for Scale Ram-Air Parachute Testing. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2019. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/446.

Council of Science Editors:

Zurita CAG. Preliminary Test Predictions for Scale Ram-Air Parachute Testing. [Masters Thesis]. Embry-Riddle Aeronautical University; 2019. Available from: https://commons.erau.edu/edt/446


Georgia Tech

15. Lambert, Thomas John. Aerodynamic control of flow dynamics coupled to a free-flight axisymmetric body.

Degree: PhD, Mechanical Engineering, 2016, Georgia Tech

 This research focuses on the unsteady flow mechanisms of using aerodynamic flow control at the aft end flow boundary of a bluff body to modify… (more)

Subjects/Keywords: Flow control; Fluid mechanics; Aerodynamics

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APA (6th Edition):

Lambert, T. J. (2016). Aerodynamic control of flow dynamics coupled to a free-flight axisymmetric body. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/56356

Chicago Manual of Style (16th Edition):

Lambert, Thomas John. “Aerodynamic control of flow dynamics coupled to a free-flight axisymmetric body.” 2016. Doctoral Dissertation, Georgia Tech. Accessed February 23, 2020. http://hdl.handle.net/1853/56356.

MLA Handbook (7th Edition):

Lambert, Thomas John. “Aerodynamic control of flow dynamics coupled to a free-flight axisymmetric body.” 2016. Web. 23 Feb 2020.

Vancouver:

Lambert TJ. Aerodynamic control of flow dynamics coupled to a free-flight axisymmetric body. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2020 Feb 23]. Available from: http://hdl.handle.net/1853/56356.

Council of Science Editors:

Lambert TJ. Aerodynamic control of flow dynamics coupled to a free-flight axisymmetric body. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/56356

16. With, Govert de. Dynamic grid adaptation applied to large eddy simulation turbulence modelling .

Degree: 2001, University of Hertfordshire

 At present a large number of fluid dynamics applications are found in aerospace, civil and automotive engineering, as well as medical related fields. In many… (more)

Subjects/Keywords: Aerodynamics; Fluid mechanics

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APA (6th Edition):

With, G. d. (2001). Dynamic grid adaptation applied to large eddy simulation turbulence modelling . (Thesis). University of Hertfordshire. Retrieved from http://hdl.handle.net/2299/14049

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):

With, Govert de. “Dynamic grid adaptation applied to large eddy simulation turbulence modelling .” 2001. Thesis, University of Hertfordshire. Accessed February 23, 2020. http://hdl.handle.net/2299/14049.

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

MLA Handbook (7th Edition):

With, Govert de. “Dynamic grid adaptation applied to large eddy simulation turbulence modelling .” 2001. Web. 23 Feb 2020.

Vancouver:

With Gd. Dynamic grid adaptation applied to large eddy simulation turbulence modelling . [Internet] [Thesis]. University of Hertfordshire; 2001. [cited 2020 Feb 23]. Available from: http://hdl.handle.net/2299/14049.

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

Council of Science Editors:

With Gd. Dynamic grid adaptation applied to large eddy simulation turbulence modelling . [Thesis]. University of Hertfordshire; 2001. Available from: http://hdl.handle.net/2299/14049

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


Embry-Riddle Aeronautical University

17. Gupte, Aditya Ajit. Effect of Thermally Induced Deformation in a Supersonic Combustion Facility.

Degree: Master of Aerospace Engineering, Aerospace Engineering, 2011, Embry-Riddle Aeronautical University

  Nastran and ANSYS finite element analysis (FEA) and Wind-US computational fluid dynamics (CFD) solvers are used to simulate the effect of thermal deformation on… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics; Aerospace Engineering

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APA (6th Edition):

Gupte, A. A. (2011). Effect of Thermally Induced Deformation in a Supersonic Combustion Facility. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/db-theses/308

Chicago Manual of Style (16th Edition):

Gupte, Aditya Ajit. “Effect of Thermally Induced Deformation in a Supersonic Combustion Facility.” 2011. Masters Thesis, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/db-theses/308.

MLA Handbook (7th Edition):

Gupte, Aditya Ajit. “Effect of Thermally Induced Deformation in a Supersonic Combustion Facility.” 2011. Web. 23 Feb 2020.

Vancouver:

Gupte AA. Effect of Thermally Induced Deformation in a Supersonic Combustion Facility. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2011. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/db-theses/308.

Council of Science Editors:

Gupte AA. Effect of Thermally Induced Deformation in a Supersonic Combustion Facility. [Masters Thesis]. Embry-Riddle Aeronautical University; 2011. Available from: https://commons.erau.edu/db-theses/308


Embry-Riddle Aeronautical University

18. Shulman, Vladislav. Performance Improvement through Velocity Triangle Optimization-Driven Redesign for Mitigating the Horseshoe Vortex in Axial Turbines.

Degree: MSin Aerospace Engineering, Aerospace Engineering, 2014, Embry-Riddle Aeronautical University

  Momentum differences between the neighboring streamlines at the end wall/primary flow interaction region of an axial turbine stage induce three-dimensional vortical flow structures, such… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics; Aerospace Engineering

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APA (6th Edition):

Shulman, V. (2014). Performance Improvement through Velocity Triangle Optimization-Driven Redesign for Mitigating the Horseshoe Vortex in Axial Turbines. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/183

Chicago Manual of Style (16th Edition):

Shulman, Vladislav. “Performance Improvement through Velocity Triangle Optimization-Driven Redesign for Mitigating the Horseshoe Vortex in Axial Turbines.” 2014. Masters Thesis, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/183.

MLA Handbook (7th Edition):

Shulman, Vladislav. “Performance Improvement through Velocity Triangle Optimization-Driven Redesign for Mitigating the Horseshoe Vortex in Axial Turbines.” 2014. Web. 23 Feb 2020.

Vancouver:

Shulman V. Performance Improvement through Velocity Triangle Optimization-Driven Redesign for Mitigating the Horseshoe Vortex in Axial Turbines. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2014. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/183.

Council of Science Editors:

Shulman V. Performance Improvement through Velocity Triangle Optimization-Driven Redesign for Mitigating the Horseshoe Vortex in Axial Turbines. [Masters Thesis]. Embry-Riddle Aeronautical University; 2014. Available from: https://commons.erau.edu/edt/183


Embry-Riddle Aeronautical University

19. Vizcaino, Jeff. Investigation of Pulse Detonation Engines; Theory, Design and Analysis.

Degree: MSin Aerospace Engineering, Aerospace Engineering, 2013, Embry-Riddle Aeronautical University

  Detonation and constant volume combustion has been known to the scientific community for some time but only recently has active research been done into… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics; Aerospace Engineering

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APA (6th Edition):

Vizcaino, J. (2013). Investigation of Pulse Detonation Engines; Theory, Design and Analysis. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/145

Chicago Manual of Style (16th Edition):

Vizcaino, Jeff. “Investigation of Pulse Detonation Engines; Theory, Design and Analysis.” 2013. Masters Thesis, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/145.

MLA Handbook (7th Edition):

Vizcaino, Jeff. “Investigation of Pulse Detonation Engines; Theory, Design and Analysis.” 2013. Web. 23 Feb 2020.

Vancouver:

Vizcaino J. Investigation of Pulse Detonation Engines; Theory, Design and Analysis. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2013. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/145.

Council of Science Editors:

Vizcaino J. Investigation of Pulse Detonation Engines; Theory, Design and Analysis. [Masters Thesis]. Embry-Riddle Aeronautical University; 2013. Available from: https://commons.erau.edu/edt/145


Embry-Riddle Aeronautical University

20. Roche, Julian. Aerodynamic Trade Study of Compound Helicopter Concepts.

Degree: MSin Aerospace Engineering, Graduate Studies, 2015, Embry-Riddle Aeronautical University

  The relative performance attributes of compound helicopter concepts have been examined, including their potential for meeting the requirements of several challenging mission profiles. For… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics; Aeronautical Vehicles

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APA (6th Edition):

Roche, J. (2015). Aerodynamic Trade Study of Compound Helicopter Concepts. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/237

Chicago Manual of Style (16th Edition):

Roche, Julian. “Aerodynamic Trade Study of Compound Helicopter Concepts.” 2015. Masters Thesis, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/237.

MLA Handbook (7th Edition):

Roche, Julian. “Aerodynamic Trade Study of Compound Helicopter Concepts.” 2015. Web. 23 Feb 2020.

Vancouver:

Roche J. Aerodynamic Trade Study of Compound Helicopter Concepts. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2015. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/237.

Council of Science Editors:

Roche J. Aerodynamic Trade Study of Compound Helicopter Concepts. [Masters Thesis]. Embry-Riddle Aeronautical University; 2015. Available from: https://commons.erau.edu/edt/237


Embry-Riddle Aeronautical University

21. Kapoor, Gaurav. Exploration of a Computational Fluid Dynamics Integrated Design Methodology for Potential Application to a Wind Turbine Blade.

Degree: MSin Aerospace Engineering, Aerospace Engineering, 2014, Embry-Riddle Aeronautical University

  The main purpose of this thesis is to conduct a parametric sensitivity study on the blade design of AOC 15/50 wind turbine based on… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics; Propulsion and Power

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APA (6th Edition):

Kapoor, G. (2014). Exploration of a Computational Fluid Dynamics Integrated Design Methodology for Potential Application to a Wind Turbine Blade. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/270

Chicago Manual of Style (16th Edition):

Kapoor, Gaurav. “Exploration of a Computational Fluid Dynamics Integrated Design Methodology for Potential Application to a Wind Turbine Blade.” 2014. Masters Thesis, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/270.

MLA Handbook (7th Edition):

Kapoor, Gaurav. “Exploration of a Computational Fluid Dynamics Integrated Design Methodology for Potential Application to a Wind Turbine Blade.” 2014. Web. 23 Feb 2020.

Vancouver:

Kapoor G. Exploration of a Computational Fluid Dynamics Integrated Design Methodology for Potential Application to a Wind Turbine Blade. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2014. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/270.

Council of Science Editors:

Kapoor G. Exploration of a Computational Fluid Dynamics Integrated Design Methodology for Potential Application to a Wind Turbine Blade. [Masters Thesis]. Embry-Riddle Aeronautical University; 2014. Available from: https://commons.erau.edu/edt/270


Embry-Riddle Aeronautical University

22. Aditya, Ron. Direct Adaptive Control for Stability and Command Augmentation System of an Air-Breathing Hypersonic Vehicle.

Degree: MSin Aerospace Engineering, Graduate Studies, 2015, Embry-Riddle Aeronautical University

  In this paper we explore a Direct Adaptive Control scheme for stabilizing a non-linear, physics based model of the longitudinal dynamics for an air… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics; Aerospace Engineering

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APA (6th Edition):

Aditya, R. (2015). Direct Adaptive Control for Stability and Command Augmentation System of an Air-Breathing Hypersonic Vehicle. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/191

Chicago Manual of Style (16th Edition):

Aditya, Ron. “Direct Adaptive Control for Stability and Command Augmentation System of an Air-Breathing Hypersonic Vehicle.” 2015. Masters Thesis, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/191.

MLA Handbook (7th Edition):

Aditya, Ron. “Direct Adaptive Control for Stability and Command Augmentation System of an Air-Breathing Hypersonic Vehicle.” 2015. Web. 23 Feb 2020.

Vancouver:

Aditya R. Direct Adaptive Control for Stability and Command Augmentation System of an Air-Breathing Hypersonic Vehicle. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2015. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/191.

Council of Science Editors:

Aditya R. Direct Adaptive Control for Stability and Command Augmentation System of an Air-Breathing Hypersonic Vehicle. [Masters Thesis]. Embry-Riddle Aeronautical University; 2015. Available from: https://commons.erau.edu/edt/191


Embry-Riddle Aeronautical University

23. Foo, Kam Keong. Investigation of Grid Adaptation to Reduce Computational Efforts for a 2-D Hydrogen-Fueled Dual-Mode Scramjet.

Degree: MSin Aerospace Engineering, Aerospace Engineering, 2013, Embry-Riddle Aeronautical University

  A two-dimensional dual-mode scramjet flowpath is developed and evaluated using the ANSYS Fluent density-based flow solver with various computational grids. Results are obtained for… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics; Aerospace Engineering

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APA (6th Edition):

Foo, K. K. (2013). Investigation of Grid Adaptation to Reduce Computational Efforts for a 2-D Hydrogen-Fueled Dual-Mode Scramjet. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/67

Chicago Manual of Style (16th Edition):

Foo, Kam Keong. “Investigation of Grid Adaptation to Reduce Computational Efforts for a 2-D Hydrogen-Fueled Dual-Mode Scramjet.” 2013. Masters Thesis, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/67.

MLA Handbook (7th Edition):

Foo, Kam Keong. “Investigation of Grid Adaptation to Reduce Computational Efforts for a 2-D Hydrogen-Fueled Dual-Mode Scramjet.” 2013. Web. 23 Feb 2020.

Vancouver:

Foo KK. Investigation of Grid Adaptation to Reduce Computational Efforts for a 2-D Hydrogen-Fueled Dual-Mode Scramjet. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2013. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/67.

Council of Science Editors:

Foo KK. Investigation of Grid Adaptation to Reduce Computational Efforts for a 2-D Hydrogen-Fueled Dual-Mode Scramjet. [Masters Thesis]. Embry-Riddle Aeronautical University; 2013. Available from: https://commons.erau.edu/edt/67


Embry-Riddle Aeronautical University

24. Matsumoto, Travis K. Determination of a Simplified High-Order Vortex Equation for Radial Equilibrium with CFD Verification.

Degree: MSin Aerospace Engineering, Graduate Studies, 2015, Embry-Riddle Aeronautical University

  The goal of this thesis is to determine a flow model that provides a better blade design over current design techniques utilizing a hybrid… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics; Aerospace Engineering

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APA (6th Edition):

Matsumoto, T. K. (2015). Determination of a Simplified High-Order Vortex Equation for Radial Equilibrium with CFD Verification. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/169

Chicago Manual of Style (16th Edition):

Matsumoto, Travis K. “Determination of a Simplified High-Order Vortex Equation for Radial Equilibrium with CFD Verification.” 2015. Masters Thesis, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/169.

MLA Handbook (7th Edition):

Matsumoto, Travis K. “Determination of a Simplified High-Order Vortex Equation for Radial Equilibrium with CFD Verification.” 2015. Web. 23 Feb 2020.

Vancouver:

Matsumoto TK. Determination of a Simplified High-Order Vortex Equation for Radial Equilibrium with CFD Verification. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2015. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/169.

Council of Science Editors:

Matsumoto TK. Determination of a Simplified High-Order Vortex Equation for Radial Equilibrium with CFD Verification. [Masters Thesis]. Embry-Riddle Aeronautical University; 2015. Available from: https://commons.erau.edu/edt/169


Embry-Riddle Aeronautical University

25. Santhanam, Vijay. Slosh Damping with Floating Magnetoactive Micro-Baffles.

Degree: MSin Aerospace Engineering, Aerospace Engineering, 2014, Embry-Riddle Aeronautical University

  Liquid sloshing within propellant tanks of launch vehicles and other major vehicles has been a major concern. Various methods have been utilized for the… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics; Aerospace Engineering

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APA (6th Edition):

Santhanam, V. (2014). Slosh Damping with Floating Magnetoactive Micro-Baffles. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/181

Chicago Manual of Style (16th Edition):

Santhanam, Vijay. “Slosh Damping with Floating Magnetoactive Micro-Baffles.” 2014. Masters Thesis, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/181.

MLA Handbook (7th Edition):

Santhanam, Vijay. “Slosh Damping with Floating Magnetoactive Micro-Baffles.” 2014. Web. 23 Feb 2020.

Vancouver:

Santhanam V. Slosh Damping with Floating Magnetoactive Micro-Baffles. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2014. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/181.

Council of Science Editors:

Santhanam V. Slosh Damping with Floating Magnetoactive Micro-Baffles. [Masters Thesis]. Embry-Riddle Aeronautical University; 2014. Available from: https://commons.erau.edu/edt/181


Embry-Riddle Aeronautical University

26. Ravulapati, Kartheek. Separation Bubbles and Vortex Formation in Cavity Flows.

Degree: MSin Aerospace Engineering, Graduate Studies, 2014, Embry-Riddle Aeronautical University

  This research is a computational fluid dynamic study of the formation of vortices and separation bubbles in a square cavity as well as in… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics; Computational Engineering

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APA (6th Edition):

Ravulapati, K. (2014). Separation Bubbles and Vortex Formation in Cavity Flows. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/179

Chicago Manual of Style (16th Edition):

Ravulapati, Kartheek. “Separation Bubbles and Vortex Formation in Cavity Flows.” 2014. Masters Thesis, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/179.

MLA Handbook (7th Edition):

Ravulapati, Kartheek. “Separation Bubbles and Vortex Formation in Cavity Flows.” 2014. Web. 23 Feb 2020.

Vancouver:

Ravulapati K. Separation Bubbles and Vortex Formation in Cavity Flows. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2014. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/179.

Council of Science Editors:

Ravulapati K. Separation Bubbles and Vortex Formation in Cavity Flows. [Masters Thesis]. Embry-Riddle Aeronautical University; 2014. Available from: https://commons.erau.edu/edt/179


Embry-Riddle Aeronautical University

27. Prabhakar, Nirmit. Design and Dynamic Analysis of a Variable-Sweep, Variable-Span Morphing UAV.

Degree: MSin Aerospace Engineering, Aerospace Engineering, 2014, Embry-Riddle Aeronautical University

  Morphing wings have the potential to optimize UAV performance for a variety of flight conditions and maneuvers. The ability to vary both the wing… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics; Aerospace Engineering

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APA (6th Edition):

Prabhakar, N. (2014). Design and Dynamic Analysis of a Variable-Sweep, Variable-Span Morphing UAV. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/177

Chicago Manual of Style (16th Edition):

Prabhakar, Nirmit. “Design and Dynamic Analysis of a Variable-Sweep, Variable-Span Morphing UAV.” 2014. Masters Thesis, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/177.

MLA Handbook (7th Edition):

Prabhakar, Nirmit. “Design and Dynamic Analysis of a Variable-Sweep, Variable-Span Morphing UAV.” 2014. Web. 23 Feb 2020.

Vancouver:

Prabhakar N. Design and Dynamic Analysis of a Variable-Sweep, Variable-Span Morphing UAV. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2014. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/177.

Council of Science Editors:

Prabhakar N. Design and Dynamic Analysis of a Variable-Sweep, Variable-Span Morphing UAV. [Masters Thesis]. Embry-Riddle Aeronautical University; 2014. Available from: https://commons.erau.edu/edt/177


Embry-Riddle Aeronautical University

28. Giovagnoli, Agustin A. Control Driven Scaling Effects of Motor and Rotors for Urban Air Mobility Design.

Degree: MSin Aerospace Engineering, Graduate Studies, 2018, Embry-Riddle Aeronautical University

  Through this thesis research the problem of controllability and propulsion associated with scaling-up consumer drones to vehicles that may carry significantly larger payloads, including… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics; Aerospace Engineering

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APA (6th Edition):

Giovagnoli, A. A. (2018). Control Driven Scaling Effects of Motor and Rotors for Urban Air Mobility Design. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/475

Chicago Manual of Style (16th Edition):

Giovagnoli, Agustin A. “Control Driven Scaling Effects of Motor and Rotors for Urban Air Mobility Design.” 2018. Masters Thesis, Embry-Riddle Aeronautical University. Accessed February 23, 2020. https://commons.erau.edu/edt/475.

MLA Handbook (7th Edition):

Giovagnoli, Agustin A. “Control Driven Scaling Effects of Motor and Rotors for Urban Air Mobility Design.” 2018. Web. 23 Feb 2020.

Vancouver:

Giovagnoli AA. Control Driven Scaling Effects of Motor and Rotors for Urban Air Mobility Design. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2018. [cited 2020 Feb 23]. Available from: https://commons.erau.edu/edt/475.

Council of Science Editors:

Giovagnoli AA. Control Driven Scaling Effects of Motor and Rotors for Urban Air Mobility Design. [Masters Thesis]. Embry-Riddle Aeronautical University; 2018. Available from: https://commons.erau.edu/edt/475


University of Colorado

29. Pope, David. Implementing a Loosely Coupled Fluid Structure Interaction Finite Element Model in PHASTA.

Degree: MS, Aerospace Engineering Sciences, 2015, University of Colorado

Fluid Structure Interaction problems are an important multi-physics phenomenon in the design of aerospace vehicles and other engineering applications. A variety of computational fluid(more)

Subjects/Keywords: ALE; Structural Equations; Aerodynamics and Fluid Mechanics

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APA (6th Edition):

Pope, D. (2015). Implementing a Loosely Coupled Fluid Structure Interaction Finite Element Model in PHASTA. (Masters Thesis). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/109

Chicago Manual of Style (16th Edition):

Pope, David. “Implementing a Loosely Coupled Fluid Structure Interaction Finite Element Model in PHASTA.” 2015. Masters Thesis, University of Colorado. Accessed February 23, 2020. https://scholar.colorado.edu/asen_gradetds/109.

MLA Handbook (7th Edition):

Pope, David. “Implementing a Loosely Coupled Fluid Structure Interaction Finite Element Model in PHASTA.” 2015. Web. 23 Feb 2020.

Vancouver:

Pope D. Implementing a Loosely Coupled Fluid Structure Interaction Finite Element Model in PHASTA. [Internet] [Masters thesis]. University of Colorado; 2015. [cited 2020 Feb 23]. Available from: https://scholar.colorado.edu/asen_gradetds/109.

Council of Science Editors:

Pope D. Implementing a Loosely Coupled Fluid Structure Interaction Finite Element Model in PHASTA. [Masters Thesis]. University of Colorado; 2015. Available from: https://scholar.colorado.edu/asen_gradetds/109


University of Tennessee – Knoxville

30. Quigley, John Nicholas. Hybrid Rocket Design Study Utilizing Nozzle Cooling and Aft-End Vortex Oxidizer Injection.

Degree: MS, Aerospace Engineering, 2014, University of Tennessee – Knoxville

  The current study focused on two innovations intended to reduce the cost and enhance the performance of hybrid rockets. The majority of the emphasis… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics; Propulsion and Power

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APA (6th Edition):

Quigley, J. N. (2014). Hybrid Rocket Design Study Utilizing Nozzle Cooling and Aft-End Vortex Oxidizer Injection. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/2843

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):

Quigley, John Nicholas. “Hybrid Rocket Design Study Utilizing Nozzle Cooling and Aft-End Vortex Oxidizer Injection.” 2014. Thesis, University of Tennessee – Knoxville. Accessed February 23, 2020. https://trace.tennessee.edu/utk_gradthes/2843.

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

MLA Handbook (7th Edition):

Quigley, John Nicholas. “Hybrid Rocket Design Study Utilizing Nozzle Cooling and Aft-End Vortex Oxidizer Injection.” 2014. Web. 23 Feb 2020.

Vancouver:

Quigley JN. Hybrid Rocket Design Study Utilizing Nozzle Cooling and Aft-End Vortex Oxidizer Injection. [Internet] [Thesis]. University of Tennessee – Knoxville; 2014. [cited 2020 Feb 23]. Available from: https://trace.tennessee.edu/utk_gradthes/2843.

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

Council of Science Editors:

Quigley JN. Hybrid Rocket Design Study Utilizing Nozzle Cooling and Aft-End Vortex Oxidizer Injection. [Thesis]. University of Tennessee – Knoxville; 2014. Available from: https://trace.tennessee.edu/utk_gradthes/2843

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

[1] [2] [3] [4] [5] … [20]

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