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You searched for +publisher:"Texas A&M University" +contributor:("White, Edward"). Showing records 1 – 30 of 49 total matches.

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Texas A&M University

1. Wheeler, Grant Benson. An Investigation of Alternative Methods for Measuring Static Pressure of Unitary Air Conditioners and Heat Pumps.

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

 This project was created to address an important issue currently faced by test facilities measuring static pressure for air-conditioning and heat pumps. Specifically, ASHRAE Standard… (more)

Subjects/Keywords: HVAC; ASHRAE Standard 37

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APA (6th Edition):

Wheeler, G. B. (2013). An Investigation of Alternative Methods for Measuring Static Pressure of Unitary Air Conditioners and Heat Pumps. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/151383

Chicago Manual of Style (16th Edition):

Wheeler, Grant Benson. “An Investigation of Alternative Methods for Measuring Static Pressure of Unitary Air Conditioners and Heat Pumps.” 2013. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/151383.

MLA Handbook (7th Edition):

Wheeler, Grant Benson. “An Investigation of Alternative Methods for Measuring Static Pressure of Unitary Air Conditioners and Heat Pumps.” 2013. Web. 17 Jan 2021.

Vancouver:

Wheeler GB. An Investigation of Alternative Methods for Measuring Static Pressure of Unitary Air Conditioners and Heat Pumps. [Internet] [Masters thesis]. Texas A&M University; 2013. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/151383.

Council of Science Editors:

Wheeler GB. An Investigation of Alternative Methods for Measuring Static Pressure of Unitary Air Conditioners and Heat Pumps. [Masters Thesis]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/151383


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. Cratty, Krista. Dynamic Wind Tunnel Load and Attitude Measurements Using State Estimation.

Degree: MS, Aerospace Engineering, 2017, Texas A&M University

 Sting-mounted models that undergo significant unsteady motion suffer from degraded data quality because the data is time-averaged to remove the unsteady fluctuations. However, time-averaged data… (more)

Subjects/Keywords: State Estimation; Wind Tunnel; Wind Tunnel Measurements; WB-57; Model Attitude; Kalman Filter

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APA (6th Edition):

Cratty, K. (2017). Dynamic Wind Tunnel Load and Attitude Measurements Using State Estimation. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/169617

Chicago Manual of Style (16th Edition):

Cratty, Krista. “Dynamic Wind Tunnel Load and Attitude Measurements Using State Estimation.” 2017. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/169617.

MLA Handbook (7th Edition):

Cratty, Krista. “Dynamic Wind Tunnel Load and Attitude Measurements Using State Estimation.” 2017. Web. 17 Jan 2021.

Vancouver:

Cratty K. Dynamic Wind Tunnel Load and Attitude Measurements Using State Estimation. [Internet] [Masters thesis]. Texas A&M University; 2017. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/169617.

Council of Science Editors:

Cratty K. Dynamic Wind Tunnel Load and Attitude Measurements Using State Estimation. [Masters Thesis]. Texas A&M University; 2017. Available from: http://hdl.handle.net/1969.1/169617


Texas A&M University

4. Daugherty, Matthew. Flat Oval Spiral Duct Deflection.

Degree: MS, Mechanical Engineering, 2014, Texas A&M University

 The deflection of a spiral duct depends on its flat span, gauge, pressure, and reinforcement. Furthermore, the duct weight determines the cost of installation, not… (more)

Subjects/Keywords: HVAC; Duct; Deflection

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APA (6th Edition):

Daugherty, M. (2014). Flat Oval Spiral Duct Deflection. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/152532

Chicago Manual of Style (16th Edition):

Daugherty, Matthew. “Flat Oval Spiral Duct Deflection.” 2014. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/152532.

MLA Handbook (7th Edition):

Daugherty, Matthew. “Flat Oval Spiral Duct Deflection.” 2014. Web. 17 Jan 2021.

Vancouver:

Daugherty M. Flat Oval Spiral Duct Deflection. [Internet] [Masters thesis]. Texas A&M University; 2014. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/152532.

Council of Science Editors:

Daugherty M. Flat Oval Spiral Duct Deflection. [Masters Thesis]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/152532


Texas A&M University

5. Kutz, Douglas M. An Updated Procedure for Tare and Interference Wind Tunnel Testing of Strut-Mounted Models.

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

 Despite advances in modern computing and simulation, wind tunnel testing remains the most trusted method for determining aerodynamic vehicle behavior. Corrections are applied to accurately… (more)

Subjects/Keywords: Wind tunnel; tare and interference; wall corrections; uncertainty; error analysis

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APA (6th Edition):

Kutz, D. M. (2014). An Updated Procedure for Tare and Interference Wind Tunnel Testing of Strut-Mounted Models. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/152679

Chicago Manual of Style (16th Edition):

Kutz, Douglas M. “An Updated Procedure for Tare and Interference Wind Tunnel Testing of Strut-Mounted Models.” 2014. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/152679.

MLA Handbook (7th Edition):

Kutz, Douglas M. “An Updated Procedure for Tare and Interference Wind Tunnel Testing of Strut-Mounted Models.” 2014. Web. 17 Jan 2021.

Vancouver:

Kutz DM. An Updated Procedure for Tare and Interference Wind Tunnel Testing of Strut-Mounted Models. [Internet] [Masters thesis]. Texas A&M University; 2014. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/152679.

Council of Science Editors:

Kutz DM. An Updated Procedure for Tare and Interference Wind Tunnel Testing of Strut-Mounted Models. [Masters Thesis]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/152679


Texas A&M University

6. Hwang, Seongil. Experimental Contribution Analysis of External Noise Components to the Interior Noise of an Automobile.

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

 The contribution analysis of various noise sources in the automobile interior noise is important for a well-designed vehicle with a low interior noise level. The… (more)

Subjects/Keywords: Contribution analysis; Interior noise of automobile

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APA (6th Edition):

Hwang, S. (2016). Experimental Contribution Analysis of External Noise Components to the Interior Noise of an Automobile. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/187324

Chicago Manual of Style (16th Edition):

Hwang, Seongil. “Experimental Contribution Analysis of External Noise Components to the Interior Noise of an Automobile.” 2016. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/187324.

MLA Handbook (7th Edition):

Hwang, Seongil. “Experimental Contribution Analysis of External Noise Components to the Interior Noise of an Automobile.” 2016. Web. 17 Jan 2021.

Vancouver:

Hwang S. Experimental Contribution Analysis of External Noise Components to the Interior Noise of an Automobile. [Internet] [Masters thesis]. Texas A&M University; 2016. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/187324.

Council of Science Editors:

Hwang S. Experimental Contribution Analysis of External Noise Components to the Interior Noise of an Automobile. [Masters Thesis]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/187324


Texas A&M University

7. Kocian, Travis Scott. Computational Hypersonic Boundary-Layer Stability and the Validation and Verification of EPIC.

Degree: PhD, Aerospace Engineering, 2018, Texas A&M University

 Laminar-to-turbulent transition is a process that is critical in determining the system drag and surface heating of a flight vehicle, and the ability to predict,… (more)

Subjects/Keywords: Hypersonics; stability; boundary-layer; CFD

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APA (6th Edition):

Kocian, T. S. (2018). Computational Hypersonic Boundary-Layer Stability and the Validation and Verification of EPIC. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/173633

Chicago Manual of Style (16th Edition):

Kocian, Travis Scott. “Computational Hypersonic Boundary-Layer Stability and the Validation and Verification of EPIC.” 2018. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/173633.

MLA Handbook (7th Edition):

Kocian, Travis Scott. “Computational Hypersonic Boundary-Layer Stability and the Validation and Verification of EPIC.” 2018. Web. 17 Jan 2021.

Vancouver:

Kocian TS. Computational Hypersonic Boundary-Layer Stability and the Validation and Verification of EPIC. [Internet] [Doctoral dissertation]. Texas A&M University; 2018. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/173633.

Council of Science Editors:

Kocian TS. Computational Hypersonic Boundary-Layer Stability and the Validation and Verification of EPIC. [Doctoral Dissertation]. Texas A&M University; 2018. Available from: http://hdl.handle.net/1969.1/173633


Texas A&M University

8. Castillo, Davis. Euler-Bernoulli Implementation of Spherical Anemometers for High Wind Speed Calculations via Strain Gauges.

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

 New measuring methods continue to be developed in the field of wind anemometry for various environments subject to low-speed and high-speed flows, turbulent-present flows, and… (more)

Subjects/Keywords: Wind Anemometry; Euler-Bernoulli beam; strain gauge; boundary conditions

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APA (6th Edition):

Castillo, D. (2011). Euler-Bernoulli Implementation of Spherical Anemometers for High Wind Speed Calculations via Strain Gauges. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9501

Chicago Manual of Style (16th Edition):

Castillo, Davis. “Euler-Bernoulli Implementation of Spherical Anemometers for High Wind Speed Calculations via Strain Gauges.” 2011. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9501.

MLA Handbook (7th Edition):

Castillo, Davis. “Euler-Bernoulli Implementation of Spherical Anemometers for High Wind Speed Calculations via Strain Gauges.” 2011. Web. 17 Jan 2021.

Vancouver:

Castillo D. Euler-Bernoulli Implementation of Spherical Anemometers for High Wind Speed Calculations via Strain Gauges. [Internet] [Masters thesis]. Texas A&M University; 2011. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9501.

Council of Science Editors:

Castillo D. Euler-Bernoulli Implementation of Spherical Anemometers for High Wind Speed Calculations via Strain Gauges. [Masters Thesis]. Texas A&M University; 2011. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9501


Texas A&M University

9. Kuester, Matthew. Acoustics in the Klebanoff-Saric Wind Tunnel: Background Identification, Forcing, and Active Control.

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

 Low disturbance wind tunnels, such as the Klebanoff–Saric Wind Tunnel (KSWT), offer an ideal environment to study boundary layer transition. In particular, the leading-edge receptivity… (more)

Subjects/Keywords: Acoustics; Wind Tunnel; Boundary Layer Receptivity; Active Noise Control

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APA (6th Edition):

Kuester, M. (2012). Acoustics in the Klebanoff-Saric Wind Tunnel: Background Identification, Forcing, and Active Control. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10731

Chicago Manual of Style (16th Edition):

Kuester, Matthew. “Acoustics in the Klebanoff-Saric Wind Tunnel: Background Identification, Forcing, and Active Control.” 2012. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10731.

MLA Handbook (7th Edition):

Kuester, Matthew. “Acoustics in the Klebanoff-Saric Wind Tunnel: Background Identification, Forcing, and Active Control.” 2012. Web. 17 Jan 2021.

Vancouver:

Kuester M. Acoustics in the Klebanoff-Saric Wind Tunnel: Background Identification, Forcing, and Active Control. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10731.

Council of Science Editors:

Kuester M. Acoustics in the Klebanoff-Saric Wind Tunnel: Background Identification, Forcing, and Active Control. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10731


Texas A&M University

10. Wilcox, Benjamin Jacob. Roughness Sensitivity Comparisons of Wind Turbine Blade Sections.

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

 One explanation for wind turbine power degradation is insect roughness. Historical studies on insect-induced power degradation have used simulation methods which are either unrepresentative of… (more)

Subjects/Keywords: wind turbine; power loss; insect roughness; wind tunnel testing

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APA (6th Edition):

Wilcox, B. J. (2016). Roughness Sensitivity Comparisons of Wind Turbine Blade Sections. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/159013

Chicago Manual of Style (16th Edition):

Wilcox, Benjamin Jacob. “Roughness Sensitivity Comparisons of Wind Turbine Blade Sections.” 2016. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/159013.

MLA Handbook (7th Edition):

Wilcox, Benjamin Jacob. “Roughness Sensitivity Comparisons of Wind Turbine Blade Sections.” 2016. Web. 17 Jan 2021.

Vancouver:

Wilcox BJ. Roughness Sensitivity Comparisons of Wind Turbine Blade Sections. [Internet] [Doctoral dissertation]. Texas A&M University; 2016. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/159013.

Council of Science Editors:

Wilcox BJ. Roughness Sensitivity Comparisons of Wind Turbine Blade Sections. [Doctoral Dissertation]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/159013


Texas A&M University

11. Marcotte, Evan Kelly. The Design and Development of a High Enthalpy, Hypervelocity Expansion Facility.

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

 Hypersonic vehicle development is an important problem of current national interest. Many of the key challenges, such as heat flux, are beyond our current predictive… (more)

Subjects/Keywords: expansion tunnel; aerospace engineering; facility design; hypersonics

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APA (6th Edition):

Marcotte, E. K. (2016). The Design and Development of a High Enthalpy, Hypervelocity Expansion Facility. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/159038

Chicago Manual of Style (16th Edition):

Marcotte, Evan Kelly. “The Design and Development of a High Enthalpy, Hypervelocity Expansion Facility.” 2016. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/159038.

MLA Handbook (7th Edition):

Marcotte, Evan Kelly. “The Design and Development of a High Enthalpy, Hypervelocity Expansion Facility.” 2016. Web. 17 Jan 2021.

Vancouver:

Marcotte EK. The Design and Development of a High Enthalpy, Hypervelocity Expansion Facility. [Internet] [Masters thesis]. Texas A&M University; 2016. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/159038.

Council of Science Editors:

Marcotte EK. The Design and Development of a High Enthalpy, Hypervelocity Expansion Facility. [Masters Thesis]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/159038


Texas A&M University

12. Long, Robert Raymond. Experiments on Dynamic Aeroelastic Response of Wind Turbine Blades.

Degree: PhD, Aerospace Engineering, 2017, Texas A&M University

 Wind turbine blades are growing progressively larger and lighter relative to their size, and these trends can lead to early failure due to fatigue. Effort… (more)

Subjects/Keywords: wind turbine; aeroelasticity; wind tunnel; experimental

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APA (6th Edition):

Long, R. R. (2017). Experiments on Dynamic Aeroelastic Response of Wind Turbine Blades. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/173080

Chicago Manual of Style (16th Edition):

Long, Robert Raymond. “Experiments on Dynamic Aeroelastic Response of Wind Turbine Blades.” 2017. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/173080.

MLA Handbook (7th Edition):

Long, Robert Raymond. “Experiments on Dynamic Aeroelastic Response of Wind Turbine Blades.” 2017. Web. 17 Jan 2021.

Vancouver:

Long RR. Experiments on Dynamic Aeroelastic Response of Wind Turbine Blades. [Internet] [Doctoral dissertation]. Texas A&M University; 2017. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/173080.

Council of Science Editors:

Long RR. Experiments on Dynamic Aeroelastic Response of Wind Turbine Blades. [Doctoral Dissertation]. Texas A&M University; 2017. Available from: http://hdl.handle.net/1969.1/173080


Texas A&M University

13. Duncan, Jr., Glen T. The Effects of Step Excrescences on Swept-Wing Boundary-Layer Transition.

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

 The immense fuel savings and environmental benefits of reducing aircraft skin-friction drag through laminar flow is well known. However, obtaining substantial laminar flow on an… (more)

Subjects/Keywords: step excrescences; 2-D roughness; forward-facing steps; aft-facing steps; boundary-layer transition; laminar flow; flight testing; wind tunnel testing; transport Reynolds number; crossflow instability; swept wings

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APA (6th Edition):

Duncan, Jr., G. T. (2014). The Effects of Step Excrescences on Swept-Wing Boundary-Layer Transition. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/153665

Chicago Manual of Style (16th Edition):

Duncan, Jr., Glen T. “The Effects of Step Excrescences on Swept-Wing Boundary-Layer Transition.” 2014. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/153665.

MLA Handbook (7th Edition):

Duncan, Jr., Glen T. “The Effects of Step Excrescences on Swept-Wing Boundary-Layer Transition.” 2014. Web. 17 Jan 2021.

Vancouver:

Duncan, Jr. GT. The Effects of Step Excrescences on Swept-Wing Boundary-Layer Transition. [Internet] [Doctoral dissertation]. Texas A&M University; 2014. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/153665.

Council of Science Editors:

Duncan, Jr. GT. The Effects of Step Excrescences on Swept-Wing Boundary-Layer Transition. [Doctoral Dissertation]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/153665


Texas A&M University

14. Herring, Alexander. Dynamic Pressure Improvements to Closed-Circuit Wind Tunnels with Flow Quality Analysis.

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

 Testing of aerodynamic loads on a sub-scale model has been the most accurate way to predict full-scale loads for many years. Even with modern advances… (more)

Subjects/Keywords: Aerospace; Wind tunnel; Testing; Flow uniformity; Diffuser design; Dynamic pressure

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APA (6th Edition):

Herring, A. (2015). Dynamic Pressure Improvements to Closed-Circuit Wind Tunnels with Flow Quality Analysis. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/155043

Chicago Manual of Style (16th Edition):

Herring, Alexander. “Dynamic Pressure Improvements to Closed-Circuit Wind Tunnels with Flow Quality Analysis.” 2015. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/155043.

MLA Handbook (7th Edition):

Herring, Alexander. “Dynamic Pressure Improvements to Closed-Circuit Wind Tunnels with Flow Quality Analysis.” 2015. Web. 17 Jan 2021.

Vancouver:

Herring A. Dynamic Pressure Improvements to Closed-Circuit Wind Tunnels with Flow Quality Analysis. [Internet] [Masters thesis]. Texas A&M University; 2015. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/155043.

Council of Science Editors:

Herring A. Dynamic Pressure Improvements to Closed-Circuit Wind Tunnels with Flow Quality Analysis. [Masters Thesis]. Texas A&M University; 2015. Available from: http://hdl.handle.net/1969.1/155043


Texas A&M University

15. Downs, Robert 1982-. Environmental Influences on Crossflow Instability.

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

 The laminar-to-turbulent transition process in swept-wing boundary layers is often dominated by an inflectional instability arising from crossflow. It is now known that freestream turbulence… (more)

Subjects/Keywords: boundary-layer stability; Crossflow instability

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APA (6th Edition):

Downs, R. 1. (2012). Environmental Influences on Crossflow Instability. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/148060

Chicago Manual of Style (16th Edition):

Downs, Robert 1982-. “Environmental Influences on Crossflow Instability.” 2012. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/148060.

MLA Handbook (7th Edition):

Downs, Robert 1982-. “Environmental Influences on Crossflow Instability.” 2012. Web. 17 Jan 2021.

Vancouver:

Downs R1. Environmental Influences on Crossflow Instability. [Internet] [Doctoral dissertation]. Texas A&M University; 2012. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/148060.

Council of Science Editors:

Downs R1. Environmental Influences on Crossflow Instability. [Doctoral Dissertation]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/148060


Texas A&M University

16. Schmucker, Jason. Experimental Investigation of Wind-Forced Drop Stability.

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

 The stability of drops forced by both wind and gravity is a fluid mechanics problem relevant to heat exchangers, fuel cells, and aircraft icing. To… (more)

Subjects/Keywords: drops; stability; runback; experiment; contact angle; hysteresis; adhesion

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APA (6th Edition):

Schmucker, J. (2012). Experimental Investigation of Wind-Forced Drop Stability. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11530

Chicago Manual of Style (16th Edition):

Schmucker, Jason. “Experimental Investigation of Wind-Forced Drop Stability.” 2012. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11530.

MLA Handbook (7th Edition):

Schmucker, Jason. “Experimental Investigation of Wind-Forced Drop Stability.” 2012. Web. 17 Jan 2021.

Vancouver:

Schmucker J. Experimental Investigation of Wind-Forced Drop Stability. [Internet] [Doctoral dissertation]. Texas A&M University; 2012. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11530.

Council of Science Editors:

Schmucker J. Experimental Investigation of Wind-Forced Drop Stability. [Doctoral Dissertation]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11530


Texas A&M University

17. 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

18. Monschke, Jason Andrew. Most-Critical Transient Disturbances in an Incompressible Flat-Plate Boundary Layer.

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

 Transient growth is a linear disturbance growth mechanism that plays a key role in roughness-induced boundary-layer transition. It occurs when superposed stable, non-orthogonal continuous spectrum… (more)

Subjects/Keywords: Transient growth; receptivity; transition; laminar; turbulent; BiGlobal; instability; adjoint optimization; parabolized Navier-Stokes; secondary instability; roughness

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APA (6th Edition):

Monschke, J. A. (2015). Most-Critical Transient Disturbances in an Incompressible Flat-Plate Boundary Layer. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/156395

Chicago Manual of Style (16th Edition):

Monschke, Jason Andrew. “Most-Critical Transient Disturbances in an Incompressible Flat-Plate Boundary Layer.” 2015. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/156395.

MLA Handbook (7th Edition):

Monschke, Jason Andrew. “Most-Critical Transient Disturbances in an Incompressible Flat-Plate Boundary Layer.” 2015. Web. 17 Jan 2021.

Vancouver:

Monschke JA. Most-Critical Transient Disturbances in an Incompressible Flat-Plate Boundary Layer. [Internet] [Doctoral dissertation]. Texas A&M University; 2015. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/156395.

Council of Science Editors:

Monschke JA. Most-Critical Transient Disturbances in an Incompressible Flat-Plate Boundary Layer. [Doctoral Dissertation]. Texas A&M University; 2015. Available from: http://hdl.handle.net/1969.1/156395


Texas A&M University

19. McManamen, Brianne Taylor. Velocity and Temperature Measurements in a High Mach Number Shock-Turbulence Interaction.

Degree: PhD, Aerospace Engineering, 2019, Texas A&M University

 Shock wave turbulence interactions are important problems with ubiquitous applications in high-speed flight and propulsion. The complex physical processes during the interaction are not fully… (more)

Subjects/Keywords: Shock-Turbulence Interaction; optical diagnostics; hypersonics

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APA (6th Edition):

McManamen, B. T. (2019). Velocity and Temperature Measurements in a High Mach Number Shock-Turbulence Interaction. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/188775

Chicago Manual of Style (16th Edition):

McManamen, Brianne Taylor. “Velocity and Temperature Measurements in a High Mach Number Shock-Turbulence Interaction.” 2019. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/188775.

MLA Handbook (7th Edition):

McManamen, Brianne Taylor. “Velocity and Temperature Measurements in a High Mach Number Shock-Turbulence Interaction.” 2019. Web. 17 Jan 2021.

Vancouver:

McManamen BT. Velocity and Temperature Measurements in a High Mach Number Shock-Turbulence Interaction. [Internet] [Doctoral dissertation]. Texas A&M University; 2019. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/188775.

Council of Science Editors:

McManamen BT. Velocity and Temperature Measurements in a High Mach Number Shock-Turbulence Interaction. [Doctoral Dissertation]. Texas A&M University; 2019. Available from: http://hdl.handle.net/1969.1/188775


Texas A&M University

20. Park, Jeongmoon. Characterization of Fluids and Thermal Performance of Tab-Induced Counter-Rotating Vortex Pairs on Surface Cooling.

Degree: PhD, Mechanical Engineering, 2018, Texas A&M University

 Characterization of the flow field generated by vortex generators (VGs) has been a matter of intense research in a host of applications ranging from aerodynamic… (more)

Subjects/Keywords: Counter-Rotating Vortex Pair; Vortex Generator; Particle Image Velocimetry; Infrared Thermography

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APA (6th Edition):

Park, J. (2018). Characterization of Fluids and Thermal Performance of Tab-Induced Counter-Rotating Vortex Pairs on Surface Cooling. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/188947

Chicago Manual of Style (16th Edition):

Park, Jeongmoon. “Characterization of Fluids and Thermal Performance of Tab-Induced Counter-Rotating Vortex Pairs on Surface Cooling.” 2018. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/188947.

MLA Handbook (7th Edition):

Park, Jeongmoon. “Characterization of Fluids and Thermal Performance of Tab-Induced Counter-Rotating Vortex Pairs on Surface Cooling.” 2018. Web. 17 Jan 2021.

Vancouver:

Park J. Characterization of Fluids and Thermal Performance of Tab-Induced Counter-Rotating Vortex Pairs on Surface Cooling. [Internet] [Doctoral dissertation]. Texas A&M University; 2018. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/188947.

Council of Science Editors:

Park J. Characterization of Fluids and Thermal Performance of Tab-Induced Counter-Rotating Vortex Pairs on Surface Cooling. [Doctoral Dissertation]. Texas A&M University; 2018. Available from: http://hdl.handle.net/1969.1/188947


Texas A&M University

21. 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

22. Belisle, Michael Joseph. Aerodynamic Design for Swept-wing Laminar Flow.

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

 This work describes and compares processes for swept-wing laminar flow control (SWLFC) aerody-namic design. It focuses on results obtained during the preliminary outer-mold-line (OML) design… (more)

Subjects/Keywords: aircraft; aerodynamic design; boundary-layer stability; boundary-layer transition; crossflow instability; discrete roughness elements; drag reduction; flight test; laminar flow control; natural laminar flow; swept-wing laminar flow control; wing design; wing glove

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APA (6th Edition):

Belisle, M. J. (2013). Aerodynamic Design for Swept-wing Laminar Flow. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/151655

Chicago Manual of Style (16th Edition):

Belisle, Michael Joseph. “Aerodynamic Design for Swept-wing Laminar Flow.” 2013. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/151655.

MLA Handbook (7th Edition):

Belisle, Michael Joseph. “Aerodynamic Design for Swept-wing Laminar Flow.” 2013. Web. 17 Jan 2021.

Vancouver:

Belisle MJ. Aerodynamic Design for Swept-wing Laminar Flow. [Internet] [Doctoral dissertation]. Texas A&M University; 2013. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/151655.

Council of Science Editors:

Belisle MJ. Aerodynamic Design for Swept-wing Laminar Flow. [Doctoral Dissertation]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/151655


Texas A&M University

23. Kuester, Matthew Scott. Distributed Roughness Receptivity in a Flat Plate Boundary Layer.

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

 Surface roughness can affect boundary layer transition by acting as a receptivity mechanism for transient growth. Several experiments have investigated transient growth created by discrete… (more)

Subjects/Keywords: Boundary Layers; Roughness; Transition

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APA (6th Edition):

Kuester, M. S. (2014). Distributed Roughness Receptivity in a Flat Plate Boundary Layer. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/152606

Chicago Manual of Style (16th Edition):

Kuester, Matthew Scott. “Distributed Roughness Receptivity in a Flat Plate Boundary Layer.” 2014. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/152606.

MLA Handbook (7th Edition):

Kuester, Matthew Scott. “Distributed Roughness Receptivity in a Flat Plate Boundary Layer.” 2014. Web. 17 Jan 2021.

Vancouver:

Kuester MS. Distributed Roughness Receptivity in a Flat Plate Boundary Layer. [Internet] [Doctoral dissertation]. Texas A&M University; 2014. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/152606.

Council of Science Editors:

Kuester MS. Distributed Roughness Receptivity in a Flat Plate Boundary Layer. [Doctoral Dissertation]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/152606


Texas A&M University

24. Sharp, Nicole Susanne. Hypersonic Measurements of Roughness-Induced Transient Growth.

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

 The effects of surface roughness on boundary-layer disturbance growth and laminar-to-turbulent transition are not well understood, especially in hypersonic boundary layers. The transient growth mechanism… (more)

Subjects/Keywords: fluid dynamics; boundary layer stability; laminar-to-turbulent transition; hypersonic flow; surface roughness; boundary layers; transient growth; nonmodal growth

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APA (6th Edition):

Sharp, N. S. (2014). Hypersonic Measurements of Roughness-Induced Transient Growth. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/152647

Chicago Manual of Style (16th Edition):

Sharp, Nicole Susanne. “Hypersonic Measurements of Roughness-Induced Transient Growth.” 2014. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/152647.

MLA Handbook (7th Edition):

Sharp, Nicole Susanne. “Hypersonic Measurements of Roughness-Induced Transient Growth.” 2014. Web. 17 Jan 2021.

Vancouver:

Sharp NS. Hypersonic Measurements of Roughness-Induced Transient Growth. [Internet] [Doctoral dissertation]. Texas A&M University; 2014. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/152647.

Council of Science Editors:

Sharp NS. Hypersonic Measurements of Roughness-Induced Transient Growth. [Doctoral Dissertation]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/152647


Texas A&M University

25. Mai, Chi Luong Nhat. Near-Region Modification of Total Pressure Fluctuations by a Normal Shock Wave in a Low-Density Hypersonic Wind Tunnel.

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

 Scientific understanding of the modifications to turbulence due to a normal shock wave at hypersonic speeds is lacking. The overarching research objective of this study… (more)

Subjects/Keywords: hypersonic flow; hypersonic wind tunnel; shock-turbulence interaction; shock waves; freestream turbulence; Pitot pressure

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APA (6th Edition):

Mai, C. L. N. (2014). Near-Region Modification of Total Pressure Fluctuations by a Normal Shock Wave in a Low-Density Hypersonic Wind Tunnel. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/152701

Chicago Manual of Style (16th Edition):

Mai, Chi Luong Nhat. “Near-Region Modification of Total Pressure Fluctuations by a Normal Shock Wave in a Low-Density Hypersonic Wind Tunnel.” 2014. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/152701.

MLA Handbook (7th Edition):

Mai, Chi Luong Nhat. “Near-Region Modification of Total Pressure Fluctuations by a Normal Shock Wave in a Low-Density Hypersonic Wind Tunnel.” 2014. Web. 17 Jan 2021.

Vancouver:

Mai CLN. Near-Region Modification of Total Pressure Fluctuations by a Normal Shock Wave in a Low-Density Hypersonic Wind Tunnel. [Internet] [Doctoral dissertation]. Texas A&M University; 2014. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/152701.

Council of Science Editors:

Mai CLN. Near-Region Modification of Total Pressure Fluctuations by a Normal Shock Wave in a Low-Density Hypersonic Wind Tunnel. [Doctoral Dissertation]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/152701


Texas A&M University

26. 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

27. Crawford, Brian Keith. Laminar-Turbulent Transition Due to 2-D Excrescences at 1% Chord on a Swept Wing.

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

 Laminar flow has the potential to dramatically reduce fuel consumption and/or extend the range of modern aircraft. However, before laminar-flow aircraft can be made practical,… (more)

Subjects/Keywords: laminar; transition; flight test; wind tunnel; excrescence; step; leading edge; transport aircraft

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APA (6th Edition):

Crawford, B. K. (2015). Laminar-Turbulent Transition Due to 2-D Excrescences at 1% Chord on a Swept Wing. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/154979

Chicago Manual of Style (16th Edition):

Crawford, Brian Keith. “Laminar-Turbulent Transition Due to 2-D Excrescences at 1% Chord on a Swept Wing.” 2015. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/154979.

MLA Handbook (7th Edition):

Crawford, Brian Keith. “Laminar-Turbulent Transition Due to 2-D Excrescences at 1% Chord on a Swept Wing.” 2015. Web. 17 Jan 2021.

Vancouver:

Crawford BK. Laminar-Turbulent Transition Due to 2-D Excrescences at 1% Chord on a Swept Wing. [Internet] [Doctoral dissertation]. Texas A&M University; 2015. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/154979.

Council of Science Editors:

Crawford BK. Laminar-Turbulent Transition Due to 2-D Excrescences at 1% Chord on a Swept Wing. [Doctoral Dissertation]. Texas A&M University; 2015. Available from: http://hdl.handle.net/1969.1/154979


Texas A&M University

28. Mendoza, Nicole Renee. On the Fundamental Unsteady Fluid Dynamics of Shock-Induced Flows through Ducts.

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

 Unsteady shock wave propagation through ducts has many applications, ranging from blast wave shelter design to advanced high-speed propulsion systems. The research objective of this… (more)

Subjects/Keywords: unsteady fluid dynamics; shock diffraction over convex corners; sudden area enlargement; shock propagation through ducts; shock-induced flows; turbulent

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APA (6th Edition):

Mendoza, N. R. (2013). On the Fundamental Unsteady Fluid Dynamics of Shock-Induced Flows through Ducts. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/149437

Chicago Manual of Style (16th Edition):

Mendoza, Nicole Renee. “On the Fundamental Unsteady Fluid Dynamics of Shock-Induced Flows through Ducts.” 2013. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/149437.

MLA Handbook (7th Edition):

Mendoza, Nicole Renee. “On the Fundamental Unsteady Fluid Dynamics of Shock-Induced Flows through Ducts.” 2013. Web. 17 Jan 2021.

Vancouver:

Mendoza NR. On the Fundamental Unsteady Fluid Dynamics of Shock-Induced Flows through Ducts. [Internet] [Doctoral dissertation]. Texas A&M University; 2013. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/149437.

Council of Science Editors:

Mendoza NR. On the Fundamental Unsteady Fluid Dynamics of Shock-Induced Flows through Ducts. [Doctoral Dissertation]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/149437


Texas A&M University

29. Hofferth, Jerrod William. Boundary-Layer Stability and Transition on a Flared Cone in a Mach 6 Quiet Wind Tunnel.

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

 A key remaining challenge in the design of hypersonic vehicles is the incomplete understanding of the process of boundary-layer transition. Turbulent heating rates are substantially… (more)

Subjects/Keywords: hypersonics; aerodynamics; wind tunnel testing; boundary-layer transition; instability waves; second-mode instability; hot-wire anemometry

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APA (6th Edition):

Hofferth, J. W. (2013). Boundary-Layer Stability and Transition on a Flared Cone in a Mach 6 Quiet Wind Tunnel. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/150990

Chicago Manual of Style (16th Edition):

Hofferth, Jerrod William. “Boundary-Layer Stability and Transition on a Flared Cone in a Mach 6 Quiet Wind Tunnel.” 2013. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/150990.

MLA Handbook (7th Edition):

Hofferth, Jerrod William. “Boundary-Layer Stability and Transition on a Flared Cone in a Mach 6 Quiet Wind Tunnel.” 2013. Web. 17 Jan 2021.

Vancouver:

Hofferth JW. Boundary-Layer Stability and Transition on a Flared Cone in a Mach 6 Quiet Wind Tunnel. [Internet] [Doctoral dissertation]. Texas A&M University; 2013. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/150990.

Council of Science Editors:

Hofferth JW. Boundary-Layer Stability and Transition on a Flared Cone in a Mach 6 Quiet Wind Tunnel. [Doctoral Dissertation]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/150990

30. Wilson, Joshua Kyle. Design and Analysis of a Test Rig for Modeling the Bit/Formation Interface in Petroleum Drilling Applications.

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

 Equipment failure and well deviations are prevailing contributors to production delays within the petroleum industry. Particular monetary focus is given to the drilling operations of… (more)

Subjects/Keywords: Drilling; Vibrations; BHA; Test Rig; Bit Formation Interface Law

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APA (6th Edition):

Wilson, J. K. (2013). Design and Analysis of a Test Rig for Modeling the Bit/Formation Interface in Petroleum Drilling Applications. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/149457

Chicago Manual of Style (16th Edition):

Wilson, Joshua Kyle. “Design and Analysis of a Test Rig for Modeling the Bit/Formation Interface in Petroleum Drilling Applications.” 2013. Masters Thesis, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/149457.

MLA Handbook (7th Edition):

Wilson, Joshua Kyle. “Design and Analysis of a Test Rig for Modeling the Bit/Formation Interface in Petroleum Drilling Applications.” 2013. Web. 17 Jan 2021.

Vancouver:

Wilson JK. Design and Analysis of a Test Rig for Modeling the Bit/Formation Interface in Petroleum Drilling Applications. [Internet] [Masters thesis]. Texas A&M University; 2013. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/1969.1/149457.

Council of Science Editors:

Wilson JK. Design and Analysis of a Test Rig for Modeling the Bit/Formation Interface in Petroleum Drilling Applications. [Masters Thesis]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/149457

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