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You searched for +publisher:"Texas A&M University" +contributor:("Rediniotis, Othon"). Showing records 1 – 30 of 61 total matches.

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Texas A&M University

1. Richards, John L. Transient Supersonic Methane-Air Flames.

Degree: MS, Aerospace Engineering, 2012, Texas A&M University

 The purpose of this study was to investigate the thermochemical properties of a transient supersonic flame. Creation of the transient flame was controlled by pulsing… (more)

Subjects/Keywords: Transient flame; supersonic flame; pulsed flame; schlieren flame; ICCD; pulsed combustion

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APA (6th Edition):

Richards, J. L. (2012). Transient Supersonic Methane-Air Flames. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-11168

Chicago Manual of Style (16th Edition):

Richards, John L. “Transient Supersonic Methane-Air Flames.” 2012. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-11168.

MLA Handbook (7th Edition):

Richards, John L. “Transient Supersonic Methane-Air Flames.” 2012. Web. 17 Jan 2021.

Vancouver:

Richards JL. Transient Supersonic Methane-Air Flames. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-11168.

Council of Science Editors:

Richards JL. Transient Supersonic Methane-Air Flames. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-11168


Texas A&M University

2. Stanford III, John William. Calibration and Uncertainty Analysis Method for a Pyramidal External Balance.

Degree: MS, Aerospace Engineering, 2016, Texas A&M University

 The Oran W. Nicks Low Speed Wind Tunnel (LSWT) uses a large-scale pyramidal-type balance to measure aerodynamic loads. The balance was built before computers were… (more)

Subjects/Keywords: wind tunnel; experimental aerodynamics; external balance; calibration

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APA (6th Edition):

Stanford III, J. W. (2016). Calibration and Uncertainty Analysis Method for a Pyramidal External Balance. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/157966

Chicago Manual of Style (16th Edition):

Stanford III, John William. “Calibration and Uncertainty Analysis Method for a Pyramidal External Balance.” 2016. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/157966.

MLA Handbook (7th Edition):

Stanford III, John William. “Calibration and Uncertainty Analysis Method for a Pyramidal External Balance.” 2016. Web. 17 Jan 2021.

Vancouver:

Stanford III JW. Calibration and Uncertainty Analysis Method for a Pyramidal External Balance. [Internet] [Masters thesis]. Texas A&M University; 2016. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/157966.

Council of Science Editors:

Stanford III JW. Calibration and Uncertainty Analysis Method for a Pyramidal External Balance. [Masters Thesis]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/157966


Texas A&M University

3. Babbar, Yogesh. Wind Tunnel and Flight Testing of Active Flow Control on a UAV.

Degree: MS, Aerospace Engineering, 2011, Texas A&M University

 Active flow control has been extensively explored in wind tunnel studies but successful in-flight implementation of an active flow control technology still remains a challenge.… (more)

Subjects/Keywords: UAV; active flow control; Extra 330; pulsed blowing; fluidic actuator; flight testing; wind tunnel testing; ailerons

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APA (6th Edition):

Babbar, Y. (2011). Wind Tunnel and Flight Testing of Active Flow Control on a UAV. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8003

Chicago Manual of Style (16th Edition):

Babbar, Yogesh. “Wind Tunnel and Flight Testing of Active Flow Control on a UAV.” 2011. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8003.

MLA Handbook (7th Edition):

Babbar, Yogesh. “Wind Tunnel and Flight Testing of Active Flow Control on a UAV.” 2011. Web. 17 Jan 2021.

Vancouver:

Babbar Y. Wind Tunnel and Flight Testing of Active Flow Control on a UAV. [Internet] [Masters thesis]. Texas A&M University; 2011. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8003.

Council of Science Editors:

Babbar Y. Wind Tunnel and Flight Testing of Active Flow Control on a UAV. [Masters Thesis]. Texas A&M University; 2011. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8003


Texas A&M University

4. Johnson, Shalom. Development of a Pulse Modulator for Active Flow Control in Turbomachinery.

Degree: MS, Aerospace Engineering, 2011, Texas A&M University

 In todays highly maneuverable jet aircraft designs, aircraft are required to have a propulsion system that can operate during sudden accelerations and rapid changes in… (more)

Subjects/Keywords: stall suppression; Turbomachinery; axial compressor; oscillatory blowing

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APA (6th Edition):

Johnson, S. (2011). Development of a Pulse Modulator for Active Flow Control in Turbomachinery. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8035

Chicago Manual of Style (16th Edition):

Johnson, Shalom. “Development of a Pulse Modulator for Active Flow Control in Turbomachinery.” 2011. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8035.

MLA Handbook (7th Edition):

Johnson, Shalom. “Development of a Pulse Modulator for Active Flow Control in Turbomachinery.” 2011. Web. 17 Jan 2021.

Vancouver:

Johnson S. Development of a Pulse Modulator for Active Flow Control in Turbomachinery. [Internet] [Masters thesis]. Texas A&M University; 2011. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8035.

Council of Science Editors:

Johnson S. Development of a Pulse Modulator for Active Flow Control in Turbomachinery. [Masters Thesis]. Texas A&M University; 2011. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8035


Texas A&M University

5. Loizou, Loizos. A Non-Pyramidal Rectangular-to-Trough Waveguide Transition and Pattern Reconfigurable Trough Waveguide Antenna.

Degree: MS, Electrical Engineering, 2012, Texas A&M University

 Trough waveguides (TWG) have been utilized in a variety of radio frequency (RF) and other related applications including radar, the treatment of hypothermia and in… (more)

Subjects/Keywords: Trough Waveguide Antenna; Pattern Reconfigurable Antenna; Multifunctional Antenna; Rectangular-to-Trough; Waveguide transition

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APA (6th Edition):

Loizou, L. (2012). A Non-Pyramidal Rectangular-to-Trough Waveguide Transition and Pattern Reconfigurable Trough Waveguide Antenna. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-12-8908

Chicago Manual of Style (16th Edition):

Loizou, Loizos. “A Non-Pyramidal Rectangular-to-Trough Waveguide Transition and Pattern Reconfigurable Trough Waveguide Antenna.” 2012. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2010-12-8908.

MLA Handbook (7th Edition):

Loizou, Loizos. “A Non-Pyramidal Rectangular-to-Trough Waveguide Transition and Pattern Reconfigurable Trough Waveguide Antenna.” 2012. Web. 17 Jan 2021.

Vancouver:

Loizou L. A Non-Pyramidal Rectangular-to-Trough Waveguide Transition and Pattern Reconfigurable Trough Waveguide Antenna. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-12-8908.

Council of Science Editors:

Loizou L. A Non-Pyramidal Rectangular-to-Trough Waveguide Transition and Pattern Reconfigurable Trough Waveguide Antenna. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-12-8908


Texas A&M University

6. Soodavi, Moein. Performance Study and Optimization of the Zephergy Wind Turbine.

Degree: MS, Aerospace Engineering, 2013, Texas A&M University

 There are many problems associated with small wind turbines, such as small Reynolds number and poor starting performance, that make them much more expensive than… (more)

Subjects/Keywords: Small Wind Turbines

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APA (6th Edition):

Soodavi, M. (2013). Performance Study and Optimization of the Zephergy Wind Turbine. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/151810

Chicago Manual of Style (16th Edition):

Soodavi, Moein. “Performance Study and Optimization of the Zephergy Wind Turbine.” 2013. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/151810.

MLA Handbook (7th Edition):

Soodavi, Moein. “Performance Study and Optimization of the Zephergy Wind Turbine.” 2013. Web. 17 Jan 2021.

Vancouver:

Soodavi M. Performance Study and Optimization of the Zephergy Wind Turbine. [Internet] [Masters thesis]. Texas A&M University; 2013. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/151810.

Council of Science Editors:

Soodavi M. Performance Study and Optimization of the Zephergy Wind Turbine. [Masters Thesis]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/151810


Texas A&M University

7. Semper, Michael Thomas. Examining A Hypersonic Turbulent Boundary Layer at Low Reynolds Number.

Degree: PhD, Aerospace Engineering, 2013, Texas A&M University

 The purpose of the current study was to answer several questions related to hypersonic, low Reynolds number, turbulent boundary layers, of which available data related… (more)

Subjects/Keywords: hypersonic; turbulent; boundary layer; low Reynolds number; experimental

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APA (6th Edition):

Semper, M. T. (2013). Examining A Hypersonic Turbulent Boundary Layer at Low Reynolds Number. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/150983

Chicago Manual of Style (16th Edition):

Semper, Michael Thomas. “Examining A Hypersonic Turbulent Boundary Layer at Low Reynolds Number.” 2013. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/150983.

MLA Handbook (7th Edition):

Semper, Michael Thomas. “Examining A Hypersonic Turbulent Boundary Layer at Low Reynolds Number.” 2013. Web. 17 Jan 2021.

Vancouver:

Semper MT. Examining A Hypersonic Turbulent Boundary Layer at Low Reynolds Number. [Internet] [Doctoral dissertation]. Texas A&M University; 2013. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/150983.

Council of Science Editors:

Semper MT. Examining A Hypersonic Turbulent Boundary Layer at Low Reynolds Number. [Doctoral Dissertation]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/150983


Texas A&M University

8. Weber, Jamie. Passive Flow Control Method for Mitigation of Unsteady Load Excursions on a Wind Turbine Blade.

Degree: MS, Aerospace Engineering, 2012, Texas A&M University

 Stochastic flow conditions, such as large unsteady wind gusts and coherent structures in turbulent winds, cause detrimental blade loadings to horizontal axis wind turbines (HAWT).… (more)

Subjects/Keywords: unsteady aerodynamics; flow control; wind turbine blade

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APA (6th Edition):

Weber, J. (2012). Passive Flow Control Method for Mitigation of Unsteady Load Excursions on a Wind Turbine Blade. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/156350

Chicago Manual of Style (16th Edition):

Weber, Jamie. “Passive Flow Control Method for Mitigation of Unsteady Load Excursions on a Wind Turbine Blade.” 2012. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/156350.

MLA Handbook (7th Edition):

Weber, Jamie. “Passive Flow Control Method for Mitigation of Unsteady Load Excursions on a Wind Turbine Blade.” 2012. Web. 17 Jan 2021.

Vancouver:

Weber J. Passive Flow Control Method for Mitigation of Unsteady Load Excursions on a Wind Turbine Blade. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/156350.

Council of Science Editors:

Weber J. Passive Flow Control Method for Mitigation of Unsteady Load Excursions on a Wind Turbine Blade. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/156350


Texas A&M University

9. Peltier, Scott Jacob. Behavior of Turbulent Structures within a Mach 5 Mechanically Distorted Boundary Layer.

Degree: PhD, Aerospace Engineering, 2013, Texas A&M University

 High-resolution particle image velocimetry (PIV) is employed to resolve the velocity fields within a Mach 4.9 mechanically distorted turbulent boundary layer (Reθ ≈ 40,000). The… (more)

Subjects/Keywords: boundary layer; turbulence; coherent structures

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APA (6th Edition):

Peltier, S. J. (2013). Behavior of Turbulent Structures within a Mach 5 Mechanically Distorted Boundary Layer. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/151397

Chicago Manual of Style (16th Edition):

Peltier, Scott Jacob. “Behavior of Turbulent Structures within a Mach 5 Mechanically Distorted Boundary Layer.” 2013. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/151397.

MLA Handbook (7th Edition):

Peltier, Scott Jacob. “Behavior of Turbulent Structures within a Mach 5 Mechanically Distorted Boundary Layer.” 2013. Web. 17 Jan 2021.

Vancouver:

Peltier SJ. Behavior of Turbulent Structures within a Mach 5 Mechanically Distorted Boundary Layer. [Internet] [Doctoral dissertation]. Texas A&M University; 2013. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/151397.

Council of Science Editors:

Peltier SJ. Behavior of Turbulent Structures within a Mach 5 Mechanically Distorted Boundary Layer. [Doctoral Dissertation]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/151397


Texas A&M University

10. Suryakumar, Vishvas Samuel. Fly-by-Feel Aeroservoelasticity.

Degree: PhD, Aerospace Engineering, 2016, Texas A&M University

 Recent experiments have suggested a strong correlation between local flow features on the airfoil surface such as the leading edge stagnation point (LESP), transition or… (more)

Subjects/Keywords: Aeroservoelasticity; Unsteady Aerodynamics; Flutter Suppression

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APA (6th Edition):

Suryakumar, V. S. (2016). Fly-by-Feel Aeroservoelasticity. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/159084

Chicago Manual of Style (16th Edition):

Suryakumar, Vishvas Samuel. “Fly-by-Feel Aeroservoelasticity.” 2016. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/159084.

MLA Handbook (7th Edition):

Suryakumar, Vishvas Samuel. “Fly-by-Feel Aeroservoelasticity.” 2016. Web. 17 Jan 2021.

Vancouver:

Suryakumar VS. Fly-by-Feel Aeroservoelasticity. [Internet] [Doctoral dissertation]. Texas A&M University; 2016. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/159084.

Council of Science Editors:

Suryakumar VS. Fly-by-Feel Aeroservoelasticity. [Doctoral Dissertation]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/159084


Texas A&M University

11. Ehrmann, Robert Schaefer. Effect of Surface Roughness on Wind Turbine Performance.

Degree: PhD, Aerospace Engineering, 2014, Texas A&M University

 Wind farm operators observe production deficits as machines age. Quantifying deterioration on individual components is difficult, but one potential explanation is accumulation of blade surface… (more)

Subjects/Keywords: roughness; boundary-layer transition; wind turbine; airfoil performance

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APA (6th Edition):

Ehrmann, R. S. (2014). Effect of Surface Roughness on Wind Turbine Performance. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/153342

Chicago Manual of Style (16th Edition):

Ehrmann, Robert Schaefer. “Effect of Surface Roughness on Wind Turbine Performance.” 2014. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/153342.

MLA Handbook (7th Edition):

Ehrmann, Robert Schaefer. “Effect of Surface Roughness on Wind Turbine Performance.” 2014. Web. 17 Jan 2021.

Vancouver:

Ehrmann RS. Effect of Surface Roughness on Wind Turbine Performance. [Internet] [Doctoral dissertation]. Texas A&M University; 2014. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/153342.

Council of Science Editors:

Ehrmann RS. Effect of Surface Roughness on Wind Turbine Performance. [Doctoral Dissertation]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/153342


Texas A&M University

12. Carpenter IV, Forrest Lafon. Practical Aspects of Computational Fluid Dynamics for Turbomachinery.

Degree: PhD, Aerospace Engineering, 2016, Texas A&M University

 The following dissertation examines several aspects of numerical simulations for turbomachinery flows modeled with an in-house Reynolds-averaged Navier-Stokes solver. The impact of the turbulence model… (more)

Subjects/Keywords: Computational Fluid Dynamcs; Turbomachinery

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APA (6th Edition):

Carpenter IV, F. L. (2016). Practical Aspects of Computational Fluid Dynamics for Turbomachinery. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/158055

Chicago Manual of Style (16th Edition):

Carpenter IV, Forrest Lafon. “Practical Aspects of Computational Fluid Dynamics for Turbomachinery.” 2016. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/158055.

MLA Handbook (7th Edition):

Carpenter IV, Forrest Lafon. “Practical Aspects of Computational Fluid Dynamics for Turbomachinery.” 2016. Web. 17 Jan 2021.

Vancouver:

Carpenter IV FL. Practical Aspects of Computational Fluid Dynamics for Turbomachinery. [Internet] [Doctoral dissertation]. Texas A&M University; 2016. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/158055.

Council of Science Editors:

Carpenter IV FL. Practical Aspects of Computational Fluid Dynamics for Turbomachinery. [Doctoral Dissertation]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/158055

13. Vannelli, Rachel Renee. Particle Image Velocimetry Near the Leading Edge of a Sikorsky SSC-A09 Wing During Dynamic Stall.

Degree: MS, Aerospace Engineering, 2012, Texas A&M University

 Dynamic stall has proven to be a complex problem in helicopter aerodynamics because it limits the helicopter flight regime. Dynamic stall is characterized by drastic… (more)

Subjects/Keywords: helicopters; dynamic stall; sikorsky; ssc-a09; particle image velocimetry; PIV

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APA (6th Edition):

Vannelli, R. R. (2012). Particle Image Velocimetry Near the Leading Edge of a Sikorsky SSC-A09 Wing During Dynamic Stall. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10510

Chicago Manual of Style (16th Edition):

Vannelli, Rachel Renee. “Particle Image Velocimetry Near the Leading Edge of a Sikorsky SSC-A09 Wing During Dynamic Stall.” 2012. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10510.

MLA Handbook (7th Edition):

Vannelli, Rachel Renee. “Particle Image Velocimetry Near the Leading Edge of a Sikorsky SSC-A09 Wing During Dynamic Stall.” 2012. Web. 17 Jan 2021.

Vancouver:

Vannelli RR. Particle Image Velocimetry Near the Leading Edge of a Sikorsky SSC-A09 Wing During Dynamic Stall. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10510.

Council of Science Editors:

Vannelli RR. Particle Image Velocimetry Near the Leading Edge of a Sikorsky SSC-A09 Wing During Dynamic Stall. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10510

14. Hidore, John Preston. Investigation of Data Quality for Wind Tunnel Internal Balance Testing.

Degree: MS, Aerospace Engineering, 2013, Texas A&M University

 Achieving high quality, consistency, and testing efficiency in wind tunnel tests using internal balances is accomplished through the use of new testing methods, analysis of… (more)

Subjects/Keywords: Data; Quality; Wind; Tunnel; Internal; Balance

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APA (6th Edition):

Hidore, J. P. (2013). Investigation of Data Quality for Wind Tunnel Internal Balance Testing. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/149384

Chicago Manual of Style (16th Edition):

Hidore, John Preston. “Investigation of Data Quality for Wind Tunnel Internal Balance Testing.” 2013. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/149384.

MLA Handbook (7th Edition):

Hidore, John Preston. “Investigation of Data Quality for Wind Tunnel Internal Balance Testing.” 2013. Web. 17 Jan 2021.

Vancouver:

Hidore JP. Investigation of Data Quality for Wind Tunnel Internal Balance Testing. [Internet] [Masters thesis]. Texas A&M University; 2013. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/149384.

Council of Science Editors:

Hidore JP. Investigation of Data Quality for Wind Tunnel Internal Balance Testing. [Masters Thesis]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/149384

15. Brenner, Thomas Andrew. Practical Aspects of the Implementation of Reduced-Order Models Based on Proper Orthogonal Decomposition.

Degree: PhD, Aerospace Engineering, 2012, Texas A&M University

 This work presents a number of the practical aspects of developing reduced- order models (ROMs) based on proper orthogonal decomposition (POD). ROMS are derived and… (more)

Subjects/Keywords: computational fluid dynamics; reduced-order modeling; proper orthogonal decomposition; multiphase flow; moving discontinuities; fluid dynamics

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APA (6th Edition):

Brenner, T. A. (2012). Practical Aspects of the Implementation of Reduced-Order Models Based on Proper Orthogonal Decomposition. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9235

Chicago Manual of Style (16th Edition):

Brenner, Thomas Andrew. “Practical Aspects of the Implementation of Reduced-Order Models Based on Proper Orthogonal Decomposition.” 2012. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9235.

MLA Handbook (7th Edition):

Brenner, Thomas Andrew. “Practical Aspects of the Implementation of Reduced-Order Models Based on Proper Orthogonal Decomposition.” 2012. Web. 17 Jan 2021.

Vancouver:

Brenner TA. Practical Aspects of the Implementation of Reduced-Order Models Based on Proper Orthogonal Decomposition. [Internet] [Doctoral dissertation]. Texas A&M University; 2012. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9235.

Council of Science Editors:

Brenner TA. Practical Aspects of the Implementation of Reduced-Order Models Based on Proper Orthogonal Decomposition. [Doctoral Dissertation]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9235

16. Guthery, John. Assessment of Flow Efficiency Through a Closed Circuit Wind Tunnel with Recommendations for Improvements.

Degree: MS, Aerospace Engineering, 2013, Texas A&M University

 Wind tunnels are designed for a certain range of test velocities and model sizes. The Oran W. Nicks Low Speed Wind Tunnel (LSWT) at Texas(more)

Subjects/Keywords: Wind Tunnel; Aerospace; Diffuser; Turning Vanes; Design

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APA (6th Edition):

Guthery, J. (2013). Assessment of Flow Efficiency Through a Closed Circuit Wind Tunnel with Recommendations for Improvements. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/151764

Chicago Manual of Style (16th Edition):

Guthery, John. “Assessment of Flow Efficiency Through a Closed Circuit Wind Tunnel with Recommendations for Improvements.” 2013. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/151764.

MLA Handbook (7th Edition):

Guthery, John. “Assessment of Flow Efficiency Through a Closed Circuit Wind Tunnel with Recommendations for Improvements.” 2013. Web. 17 Jan 2021.

Vancouver:

Guthery J. Assessment of Flow Efficiency Through a Closed Circuit Wind Tunnel with Recommendations for Improvements. [Internet] [Masters thesis]. Texas A&M University; 2013. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/151764.

Council of Science Editors:

Guthery J. Assessment of Flow Efficiency Through a Closed Circuit Wind Tunnel with Recommendations for Improvements. [Masters Thesis]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/151764

17. Kirk, Aaron Michael. Active flow control in an advanced serpentine jet engine inlet duct.

Degree: MS, Aerospace Engineering, 2009, Texas A&M University

 An experimental investigation was performed to understand the development and suppression of the secondary flow structures within a compact, serpentine jet engine inlet duct. By… (more)

Subjects/Keywords: serpentine; duct; flow control; SJA; secondary flow; inlet; synthetic jet actuator; s-duct

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APA (6th Edition):

Kirk, A. M. (2009). Active flow control in an advanced serpentine jet engine inlet duct. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1027

Chicago Manual of Style (16th Edition):

Kirk, Aaron Michael. “Active flow control in an advanced serpentine jet engine inlet duct.” 2009. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-1027.

MLA Handbook (7th Edition):

Kirk, Aaron Michael. “Active flow control in an advanced serpentine jet engine inlet duct.” 2009. Web. 17 Jan 2021.

Vancouver:

Kirk AM. Active flow control in an advanced serpentine jet engine inlet duct. [Internet] [Masters thesis]. Texas A&M University; 2009. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1027.

Council of Science Editors:

Kirk AM. Active flow control in an advanced serpentine jet engine inlet duct. [Masters Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1027

18. Banerjee, Arindam. Statistically steady measurements of Rayleigh-Taylor mixing in a gas channel.

Degree: PhD, Mechanical Engineering, 2006, Texas A&M University

 A novel gas channel experiment was constructed to study the development of high Atwood number Rayleigh-Taylor mixing. Two gas streams, one containing air and the… (more)

Subjects/Keywords: Turbulent Flows; Bouyancy driven instabilities

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APA (6th Edition):

Banerjee, A. (2006). Statistically steady measurements of Rayleigh-Taylor mixing in a gas channel. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/4183

Chicago Manual of Style (16th Edition):

Banerjee, Arindam. “Statistically steady measurements of Rayleigh-Taylor mixing in a gas channel.” 2006. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/4183.

MLA Handbook (7th Edition):

Banerjee, Arindam. “Statistically steady measurements of Rayleigh-Taylor mixing in a gas channel.” 2006. Web. 17 Jan 2021.

Vancouver:

Banerjee A. Statistically steady measurements of Rayleigh-Taylor mixing in a gas channel. [Internet] [Doctoral dissertation]. Texas A&M University; 2006. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/4183.

Council of Science Editors:

Banerjee A. Statistically steady measurements of Rayleigh-Taylor mixing in a gas channel. [Doctoral Dissertation]. Texas A&M University; 2006. Available from: http://hdl.handle.net/1969.1/4183

19. Ravi, Gurunarayana. Study of Laminar Flow Forced Convection Heat Transfer Behavior of a Phase Change Material Fluid.

Degree: MS, Mechanical Engineering, 2010, Texas A&M University

 The heat transfer behavior of phase change material fluid under laminar flow conditions in circular tubes and internally longitudinal finned tubes are presented in this… (more)

Subjects/Keywords: longitudinal internal fins; phase change material; laminar flow; enhanced heat transfer; finned tube; H1 boundary condition; H2 boundary condition; PCM; MPCM; FLUENT; finned tube

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APA (6th Edition):

Ravi, G. (2010). Study of Laminar Flow Forced Convection Heat Transfer Behavior of a Phase Change Material Fluid. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2008-12-231

Chicago Manual of Style (16th Edition):

Ravi, Gurunarayana. “Study of Laminar Flow Forced Convection Heat Transfer Behavior of a Phase Change Material Fluid.” 2010. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2008-12-231.

MLA Handbook (7th Edition):

Ravi, Gurunarayana. “Study of Laminar Flow Forced Convection Heat Transfer Behavior of a Phase Change Material Fluid.” 2010. Web. 17 Jan 2021.

Vancouver:

Ravi G. Study of Laminar Flow Forced Convection Heat Transfer Behavior of a Phase Change Material Fluid. [Internet] [Masters thesis]. Texas A&M University; 2010. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2008-12-231.

Council of Science Editors:

Ravi G. Study of Laminar Flow Forced Convection Heat Transfer Behavior of a Phase Change Material Fluid. [Masters Thesis]. Texas A&M University; 2010. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2008-12-231

20. Kumar, Abhinav. Flow control optimization in a jet engine serpentine inlet duct.

Degree: MS, Aerospace Engineering, 2009, Texas A&M University

 Computational investigations were carried out on an advanced serpentine jet engine inlet duct to understand the development and propagation of secondary flow structures. Computational analysis… (more)

Subjects/Keywords: flow control; aerodynamics; inlet duct

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APA (6th Edition):

Kumar, A. (2009). Flow control optimization in a jet engine serpentine inlet duct. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1399

Chicago Manual of Style (16th Edition):

Kumar, Abhinav. “Flow control optimization in a jet engine serpentine inlet duct.” 2009. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-1399.

MLA Handbook (7th Edition):

Kumar, Abhinav. “Flow control optimization in a jet engine serpentine inlet duct.” 2009. Web. 17 Jan 2021.

Vancouver:

Kumar A. Flow control optimization in a jet engine serpentine inlet duct. [Internet] [Masters thesis]. Texas A&M University; 2009. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1399.

Council of Science Editors:

Kumar A. Flow control optimization in a jet engine serpentine inlet duct. [Masters Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1399

21. Tichenor, Nathan R. Characterization of the Influence of a Favorable Pressure Gradient on the Basic Structure of a Mach 5.0 High Reynolds Number Supersonic Turbulent Boundary Layer.

Degree: PhD, Aerospace Engineering, 2010, Texas A&M University

 High-speed high Reynolds number boundary layer flows with mechanical non-equilibrium effects have numerous practical applications; examples include access-to-space ascent, re-entry and descent, and military hypersonic… (more)

Subjects/Keywords: hypersonic; Mach 5.0; favorable pressure gradient

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APA (6th Edition):

Tichenor, N. R. (2010). Characterization of the Influence of a Favorable Pressure Gradient on the Basic Structure of a Mach 5.0 High Reynolds Number Supersonic Turbulent Boundary Layer. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8407

Chicago Manual of Style (16th Edition):

Tichenor, Nathan R. “Characterization of the Influence of a Favorable Pressure Gradient on the Basic Structure of a Mach 5.0 High Reynolds Number Supersonic Turbulent Boundary Layer.” 2010. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8407.

MLA Handbook (7th Edition):

Tichenor, Nathan R. “Characterization of the Influence of a Favorable Pressure Gradient on the Basic Structure of a Mach 5.0 High Reynolds Number Supersonic Turbulent Boundary Layer.” 2010. Web. 17 Jan 2021.

Vancouver:

Tichenor NR. Characterization of the Influence of a Favorable Pressure Gradient on the Basic Structure of a Mach 5.0 High Reynolds Number Supersonic Turbulent Boundary Layer. [Internet] [Doctoral dissertation]. Texas A&M University; 2010. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8407.

Council of Science Editors:

Tichenor NR. Characterization of the Influence of a Favorable Pressure Gradient on the Basic Structure of a Mach 5.0 High Reynolds Number Supersonic Turbulent Boundary Layer. [Doctoral Dissertation]. Texas A&M University; 2010. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8407

22. Kluzek, Celine D. Structure of Partially Premixed Flames Using Detailed Chemistry Simulations.

Degree: PhD, Aerospace Engineering, 2010, Texas A&M University

 State-of-the-art reacting-flow computations have to compromise either on the detail of chemical reactions or on the dimensionality of the solution, while experiments in flames are… (more)

Subjects/Keywords: partially premixed flames; Cantera; cross-transport

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APA (6th Edition):

Kluzek, C. D. (2010). Structure of Partially Premixed Flames Using Detailed Chemistry Simulations. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-3276

Chicago Manual of Style (16th Edition):

Kluzek, Celine D. “Structure of Partially Premixed Flames Using Detailed Chemistry Simulations.” 2010. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-3276.

MLA Handbook (7th Edition):

Kluzek, Celine D. “Structure of Partially Premixed Flames Using Detailed Chemistry Simulations.” 2010. Web. 17 Jan 2021.

Vancouver:

Kluzek CD. Structure of Partially Premixed Flames Using Detailed Chemistry Simulations. [Internet] [Doctoral dissertation]. Texas A&M University; 2010. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-3276.

Council of Science Editors:

Kluzek CD. Structure of Partially Premixed Flames Using Detailed Chemistry Simulations. [Doctoral Dissertation]. Texas A&M University; 2010. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-3276

23. Ekoto, Isaac Wesley. Supersonic turbulent boundary layers with periodic mechanical non-equilibrium.

Degree: PhD, Aerospace Engineering, 2007, Texas A&M University

 Previous studies have shown that favorable pressure gradients reduce the turbulence levels and length scales in supersonic flow. Wall roughness has been shown to reduce… (more)

Subjects/Keywords: supersonic; turbulent; boundary layer; roughness; favorable pressure gradient

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APA (6th Edition):

Ekoto, I. W. (2007). Supersonic turbulent boundary layers with periodic mechanical non-equilibrium. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/4709

Chicago Manual of Style (16th Edition):

Ekoto, Isaac Wesley. “Supersonic turbulent boundary layers with periodic mechanical non-equilibrium.” 2007. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/4709.

MLA Handbook (7th Edition):

Ekoto, Isaac Wesley. “Supersonic turbulent boundary layers with periodic mechanical non-equilibrium.” 2007. Web. 17 Jan 2021.

Vancouver:

Ekoto IW. Supersonic turbulent boundary layers with periodic mechanical non-equilibrium. [Internet] [Doctoral dissertation]. Texas A&M University; 2007. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/4709.

Council of Science Editors:

Ekoto IW. Supersonic turbulent boundary layers with periodic mechanical non-equilibrium. [Doctoral Dissertation]. Texas A&M University; 2007. Available from: http://hdl.handle.net/1969.1/4709

24. Watanawanavet, Somsak. CFD optimization study of high-efficiency jet ejectors.

Degree: PhD, Chemical Engineering, 2009, Texas A&M University

 Research was performed to optimize the high-efficiency jet ejector geometry by varying motive velocities from Mach 0.50 to 3.25, and mass flow ratio from 0.02… (more)

Subjects/Keywords: High-Efficiency Jet Ejector

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APA (6th Edition):

Watanawanavet, S. (2009). CFD optimization study of high-efficiency jet ejectors. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2387

Chicago Manual of Style (16th Edition):

Watanawanavet, Somsak. “CFD optimization study of high-efficiency jet ejectors.” 2009. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2387.

MLA Handbook (7th Edition):

Watanawanavet, Somsak. “CFD optimization study of high-efficiency jet ejectors.” 2009. Web. 17 Jan 2021.

Vancouver:

Watanawanavet S. CFD optimization study of high-efficiency jet ejectors. [Internet] [Doctoral dissertation]. Texas A&M University; 2009. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2387.

Council of Science Editors:

Watanawanavet S. CFD optimization study of high-efficiency jet ejectors. [Doctoral Dissertation]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2387

25. Majji, Manoranjan. Robust control of redundantly actuated dynamical systems.

Degree: MS, Aerospace Engineering, 2006, Texas A&M University

 The eigenstructure assignment scheme for robust multivariable feedback control is extended to redundantly actuated dynamical systems. It is shown that an orthonormal set of close… (more)

Subjects/Keywords: Redundant Actuation; Distributed Control.

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APA (6th Edition):

Majji, M. (2006). Robust control of redundantly actuated dynamical systems. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/3889

Chicago Manual of Style (16th Edition):

Majji, Manoranjan. “Robust control of redundantly actuated dynamical systems.” 2006. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/3889.

MLA Handbook (7th Edition):

Majji, Manoranjan. “Robust control of redundantly actuated dynamical systems.” 2006. Web. 17 Jan 2021.

Vancouver:

Majji M. Robust control of redundantly actuated dynamical systems. [Internet] [Masters thesis]. Texas A&M University; 2006. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/3889.

Council of Science Editors:

Majji M. Robust control of redundantly actuated dynamical systems. [Masters Thesis]. Texas A&M University; 2006. Available from: http://hdl.handle.net/1969.1/3889

26. Joly, Michael Marie. Multifidelity, Multidisciplinary Optimization of Turbomachines with Shock Interaction.

Degree: PhD, Aerospace Engineering, 2014, Texas A&M University

 Research on high-speed air-breathing propulsion aims at developing aircraft with antipodal range and space access. Before reaching high speed at high altitude, the flight vehicle… (more)

Subjects/Keywords: Turbomachinery; Optimization

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APA (6th Edition):

Joly, M. M. (2014). Multifidelity, Multidisciplinary Optimization of Turbomachines with Shock Interaction. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/153360

Chicago Manual of Style (16th Edition):

Joly, Michael Marie. “Multifidelity, Multidisciplinary Optimization of Turbomachines with Shock Interaction.” 2014. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/153360.

MLA Handbook (7th Edition):

Joly, Michael Marie. “Multifidelity, Multidisciplinary Optimization of Turbomachines with Shock Interaction.” 2014. Web. 17 Jan 2021.

Vancouver:

Joly MM. Multifidelity, Multidisciplinary Optimization of Turbomachines with Shock Interaction. [Internet] [Doctoral dissertation]. Texas A&M University; 2014. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/153360.

Council of Science Editors:

Joly MM. Multifidelity, Multidisciplinary Optimization of Turbomachines with Shock Interaction. [Doctoral Dissertation]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/153360

27. Babbar, Yogesh. Aeroelastic Response of a Typical Wing Section under Nonlinearities and Gust Loads.

Degree: PhD, Aerospace Engineering, 2015, Texas A&M University

 Aeroservoelasticity (ASE) is the interdisciplinary study of the interaction of structural, inertial, aerodynamic, and control loads for aircraft systems, and is inherently a nonlinear phenomenon.… (more)

Subjects/Keywords: aeroelasticity; aeroservoelasticity; aeroelastic response; gust loads; nonlinear; nonlinearity; LCO; flutter; bifurcation; hopf

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APA (6th Edition):

Babbar, Y. (2015). Aeroelastic Response of a Typical Wing Section under Nonlinearities and Gust Loads. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/155296

Chicago Manual of Style (16th Edition):

Babbar, Yogesh. “Aeroelastic Response of a Typical Wing Section under Nonlinearities and Gust Loads.” 2015. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/155296.

MLA Handbook (7th Edition):

Babbar, Yogesh. “Aeroelastic Response of a Typical Wing Section under Nonlinearities and Gust Loads.” 2015. Web. 17 Jan 2021.

Vancouver:

Babbar Y. Aeroelastic Response of a Typical Wing Section under Nonlinearities and Gust Loads. [Internet] [Doctoral dissertation]. Texas A&M University; 2015. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/155296.

Council of Science Editors:

Babbar Y. Aeroelastic Response of a Typical Wing Section under Nonlinearities and Gust Loads. [Doctoral Dissertation]. Texas A&M University; 2015. Available from: http://hdl.handle.net/1969.1/155296


Texas A&M University

28. Sahoo, Dipankar. Experimental analysis of the vorticity and turbulent flow dynamics of a pitching airfoil at realistic flight (helicopter) conditions.

Degree: PhD, Aerospace Engineering, 2008, Texas A&M University

 Improved basic understanding, predictability, and controllability of vortex-dominated and unsteady aerodynamic flows are important in enhancement of the performance of next generation helicopters. The primary… (more)

Subjects/Keywords: Dynamic Stall; NACA 0012; Turbulent Flow Field; Reynolds Shear Stress; Production of Turbulence; Time Scale; PIV

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APA (6th Edition):

Sahoo, D. (2008). Experimental analysis of the vorticity and turbulent flow dynamics of a pitching airfoil at realistic flight (helicopter) conditions. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/85893

Chicago Manual of Style (16th Edition):

Sahoo, Dipankar. “Experimental analysis of the vorticity and turbulent flow dynamics of a pitching airfoil at realistic flight (helicopter) conditions.” 2008. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/85893.

MLA Handbook (7th Edition):

Sahoo, Dipankar. “Experimental analysis of the vorticity and turbulent flow dynamics of a pitching airfoil at realistic flight (helicopter) conditions.” 2008. Web. 17 Jan 2021.

Vancouver:

Sahoo D. Experimental analysis of the vorticity and turbulent flow dynamics of a pitching airfoil at realistic flight (helicopter) conditions. [Internet] [Doctoral dissertation]. Texas A&M University; 2008. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/85893.

Council of Science Editors:

Sahoo D. Experimental analysis of the vorticity and turbulent flow dynamics of a pitching airfoil at realistic flight (helicopter) conditions. [Doctoral Dissertation]. Texas A&M University; 2008. Available from: http://hdl.handle.net/1969.1/85893


Texas A&M University

29. Cohen, Benjamin Nathan. Multiscalar line measurements in nonisobaric high-pressure underexpanded supersonic jets using rotational-vibrational raman spectroscopy.

Degree: MS, Aerospace Engineering, 2009, Texas A&M University

 This work describes the development of a Raman spectroscopy system for measuring aerothermochemistry in high-speed jets and flames. A transmissive grating spectrometer was newly developed… (more)

Subjects/Keywords: Raman; Rayleigh; Laser Diagnostics; Rotational; Vibrational; Nonisobaric; Spectroscopy

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APA (6th Edition):

Cohen, B. N. (2009). Multiscalar line measurements in nonisobaric high-pressure underexpanded supersonic jets using rotational-vibrational raman spectroscopy. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2619

Chicago Manual of Style (16th Edition):

Cohen, Benjamin Nathan. “Multiscalar line measurements in nonisobaric high-pressure underexpanded supersonic jets using rotational-vibrational raman spectroscopy.” 2009. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2619.

MLA Handbook (7th Edition):

Cohen, Benjamin Nathan. “Multiscalar line measurements in nonisobaric high-pressure underexpanded supersonic jets using rotational-vibrational raman spectroscopy.” 2009. Web. 17 Jan 2021.

Vancouver:

Cohen BN. Multiscalar line measurements in nonisobaric high-pressure underexpanded supersonic jets using rotational-vibrational raman spectroscopy. [Internet] [Masters thesis]. Texas A&M University; 2009. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2619.

Council of Science Editors:

Cohen BN. Multiscalar line measurements in nonisobaric high-pressure underexpanded supersonic jets using rotational-vibrational raman spectroscopy. [Masters Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2619


Texas A&M University

30. Tichenor, Nathan Ryan. Particle image velocimetry in an advanced, serpentine jet engine inlet duct.

Degree: MS, Aerospace Engineering, 2009, Texas A&M University

 The overarching objective of this research project was to gain improved basic understanding of the fluid mechanisms governing the development of secondary flow structures in… (more)

Subjects/Keywords: PIV; Particle Image Velocimetry; Serpentine; Vorticies

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APA (6th Edition):

Tichenor, N. R. (2009). Particle image velocimetry in an advanced, serpentine jet engine inlet duct. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1401

Chicago Manual of Style (16th Edition):

Tichenor, Nathan Ryan. “Particle image velocimetry in an advanced, serpentine jet engine inlet duct.” 2009. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-1401.

MLA Handbook (7th Edition):

Tichenor, Nathan Ryan. “Particle image velocimetry in an advanced, serpentine jet engine inlet duct.” 2009. Web. 17 Jan 2021.

Vancouver:

Tichenor NR. Particle image velocimetry in an advanced, serpentine jet engine inlet duct. [Internet] [Masters thesis]. Texas A&M University; 2009. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1401.

Council of Science Editors:

Tichenor NR. Particle image velocimetry in an advanced, serpentine jet engine inlet duct. [Masters Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1401

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