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You searched for +publisher:"Texas A&M University" +contributor:("Reed, Helen"). Showing records 1 – 30 of 42 total matches.

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Texas A&M University

1. Graves, John. Small Satellite Applications of Commercial off the Shelf Radio Frequency Integrated Circuits.

Degree: 2012, Texas A&M University

 Within the first decade of the 21st century, the aerospace community has seen many more opportunities to launch small spacecraft in the 10 to 100… (more)

Subjects/Keywords: Small satellites; RFIC; downlink communications; spacecraft; university satellites

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APA (6th Edition):

Graves, J. (2012). Small Satellite Applications of Commercial off the Shelf Radio Frequency Integrated Circuits. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10387

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

Chicago Manual of Style (16th Edition):

Graves, John. “Small Satellite Applications of Commercial off the Shelf Radio Frequency Integrated Circuits.” 2012. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10387.

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

MLA Handbook (7th Edition):

Graves, John. “Small Satellite Applications of Commercial off the Shelf Radio Frequency Integrated Circuits.” 2012. Web. 21 Nov 2019.

Vancouver:

Graves J. Small Satellite Applications of Commercial off the Shelf Radio Frequency Integrated Circuits. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10387.

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

Council of Science Editors:

Graves J. Small Satellite Applications of Commercial off the Shelf Radio Frequency Integrated Circuits. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10387

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


Texas A&M University

2. Pruski, Brandon. Leading Edge Flow Structure of a Dynamically Pitching NACA 0012 Airfoil.

Degree: 2012, Texas A&M University

 The leading edge flow structure of the NACA 0012 airfoil is experimentally investigated under dynamic stall conditions (M = 0.1; ? = 16.7?, 22.4?; Rec… (more)

Subjects/Keywords: Vortex dominated flowfield; Unsteady Aerodynamics; Dynamic Stall

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APA (6th Edition):

Pruski, B. (2012). Leading Edge Flow Structure of a Dynamically Pitching NACA 0012 Airfoil. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/148372

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

Chicago Manual of Style (16th Edition):

Pruski, Brandon. “Leading Edge Flow Structure of a Dynamically Pitching NACA 0012 Airfoil.” 2012. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/148372.

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

MLA Handbook (7th Edition):

Pruski, Brandon. “Leading Edge Flow Structure of a Dynamically Pitching NACA 0012 Airfoil.” 2012. Web. 21 Nov 2019.

Vancouver:

Pruski B. Leading Edge Flow Structure of a Dynamically Pitching NACA 0012 Airfoil. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/148372.

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

Council of Science Editors:

Pruski B. Leading Edge Flow Structure of a Dynamically Pitching NACA 0012 Airfoil. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/148372

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


Texas A&M University

3. Baker, Jose Enrique. Measurements of leakage, power loss and rotordynamic force coefficients in a hybrid brush seal.

Degree: 2009, Texas A&M University

 This thesis presents measurements of power loss and leakage in a hybrid brush seal (HBS) for increasing pressure differentials and over a range of rotor… (more)

Subjects/Keywords: stiffness; seal

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APA (6th Edition):

Baker, J. E. (2009). Measurements of leakage, power loss and rotordynamic force coefficients in a hybrid brush seal. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2767

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

Chicago Manual of Style (16th Edition):

Baker, Jose Enrique. “Measurements of leakage, power loss and rotordynamic force coefficients in a hybrid brush seal.” 2009. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2767.

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

MLA Handbook (7th Edition):

Baker, Jose Enrique. “Measurements of leakage, power loss and rotordynamic force coefficients in a hybrid brush seal.” 2009. Web. 21 Nov 2019.

Vancouver:

Baker JE. Measurements of leakage, power loss and rotordynamic force coefficients in a hybrid brush seal. [Internet] [Thesis]. Texas A&M University; 2009. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2767.

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

Council of Science Editors:

Baker JE. Measurements of leakage, power loss and rotordynamic force coefficients in a hybrid brush seal. [Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2767

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


Texas A&M University

4. Stancliffe, Devin Aldin. Analysis and Design of a Test Apparatus for Resolving Near-Field Effects Associated With Using a Coarse Sun Sensor as Part of a 6-DOF Solution.

Degree: 2011, Texas A&M University

 Though the Aerospace industry is moving towards small satellites and smaller sensor technologies, sensors used for close-proximity operations are generally cost (and often size and… (more)

Subjects/Keywords: Coarse sun sensors; 6-dof; near-field effects; NorthStar; close-proximity; autonomous rendezvous and docking

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APA (6th Edition):

Stancliffe, D. A. (2011). Analysis and Design of a Test Apparatus for Resolving Near-Field Effects Associated With Using a Coarse Sun Sensor as Part of a 6-DOF Solution. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8440

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

Chicago Manual of Style (16th Edition):

Stancliffe, Devin Aldin. “Analysis and Design of a Test Apparatus for Resolving Near-Field Effects Associated With Using a Coarse Sun Sensor as Part of a 6-DOF Solution.” 2011. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8440.

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

MLA Handbook (7th Edition):

Stancliffe, Devin Aldin. “Analysis and Design of a Test Apparatus for Resolving Near-Field Effects Associated With Using a Coarse Sun Sensor as Part of a 6-DOF Solution.” 2011. Web. 21 Nov 2019.

Vancouver:

Stancliffe DA. Analysis and Design of a Test Apparatus for Resolving Near-Field Effects Associated With Using a Coarse Sun Sensor as Part of a 6-DOF Solution. [Internet] [Thesis]. Texas A&M University; 2011. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8440.

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

Council of Science Editors:

Stancliffe DA. Analysis and Design of a Test Apparatus for Resolving Near-Field Effects Associated With Using a Coarse Sun Sensor as Part of a 6-DOF Solution. [Thesis]. Texas A&M University; 2011. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8440

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


Texas A&M University

5. Hafer, William. Improvement of PNP Problem Computational Efficiency For Known Target Geometry of Cubesats.

Degree: 2012, Texas A&M University

 This thesis considers the Perspective-N-Point (PNP) problem with orthogonal target geometry, as seen in the problem of cubesat relative navigation. Cubesats are small spacecraft often… (more)

Subjects/Keywords: PNP problem; P3P problem; Known target geometry; Spacecraft relative navigation from vector measurements

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APA (6th Edition):

Hafer, W. (2012). Improvement of PNP Problem Computational Efficiency For Known Target Geometry of Cubesats. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10958

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

Chicago Manual of Style (16th Edition):

Hafer, William. “Improvement of PNP Problem Computational Efficiency For Known Target Geometry of Cubesats.” 2012. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10958.

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

MLA Handbook (7th Edition):

Hafer, William. “Improvement of PNP Problem Computational Efficiency For Known Target Geometry of Cubesats.” 2012. Web. 21 Nov 2019.

Vancouver:

Hafer W. Improvement of PNP Problem Computational Efficiency For Known Target Geometry of Cubesats. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10958.

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

Council of Science Editors:

Hafer W. Improvement of PNP Problem Computational Efficiency For Known Target Geometry of Cubesats. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10958

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


Texas A&M University

6. Rhodes, Richard G. Computations of Laminar Flow Control on Swept Wings as a Companion to Flight Test Research.

Degree: 2010, Texas A&M University

 The high cost of energy has resulted in a renewed interest in the study of reducing skin-friction drag in aeronautical applications. Laminar Flow Control (LFC)… (more)

Subjects/Keywords: laminar; turbulence; flow; control; fluent; gambit; crossflow; lastrac

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APA (6th Edition):

Rhodes, R. G. (2010). Computations of Laminar Flow Control on Swept Wings as a Companion to Flight Test Research. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2008-12-96

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

Chicago Manual of Style (16th Edition):

Rhodes, Richard G. “Computations of Laminar Flow Control on Swept Wings as a Companion to Flight Test Research.” 2010. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2008-12-96.

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

MLA Handbook (7th Edition):

Rhodes, Richard G. “Computations of Laminar Flow Control on Swept Wings as a Companion to Flight Test Research.” 2010. Web. 21 Nov 2019.

Vancouver:

Rhodes RG. Computations of Laminar Flow Control on Swept Wings as a Companion to Flight Test Research. [Internet] [Thesis]. Texas A&M University; 2010. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2008-12-96.

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

Council of Science Editors:

Rhodes RG. Computations of Laminar Flow Control on Swept Wings as a Companion to Flight Test Research. [Thesis]. Texas A&M University; 2010. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2008-12-96

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


Texas A&M University

7. McLelland, Angela N. Simulation and Experimental Predictionss for the Structural Response of Satellites.

Degree: 2013, Texas A&M University

 This research investigated the structural response of satellites and space rated payloads. Throughout the work, SolidWorks Simulation was utilized to subject the aforementioned systems to… (more)

Subjects/Keywords: satellites; CAD; structural response

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APA (6th Edition):

McLelland, A. N. (2013). Simulation and Experimental Predictionss for the Structural Response of Satellites. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/151922

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

Chicago Manual of Style (16th Edition):

McLelland, Angela N. “Simulation and Experimental Predictionss for the Structural Response of Satellites.” 2013. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/151922.

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

MLA Handbook (7th Edition):

McLelland, Angela N. “Simulation and Experimental Predictionss for the Structural Response of Satellites.” 2013. Web. 21 Nov 2019.

Vancouver:

McLelland AN. Simulation and Experimental Predictionss for the Structural Response of Satellites. [Internet] [Thesis]. Texas A&M University; 2013. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/151922.

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

Council of Science Editors:

McLelland AN. Simulation and Experimental Predictionss for the Structural Response of Satellites. [Thesis]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/151922

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


Texas A&M University

8. Shao, Qi. Surface Signature of Flow Past a Sphere at Moderate Reynolds Numbers.

Degree: 2014, Texas A&M University

 The incompressible viscous flow past a sphere is investigated numerically at moderate Reynolds numbers. Periodic vortex shedding happens at these Reynolds numbers. The primary objective… (more)

Subjects/Keywords: Sphere; DNS; incompressible

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APA (6th Edition):

Shao, Q. (2014). Surface Signature of Flow Past a Sphere at Moderate Reynolds Numbers. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/152601

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

Chicago Manual of Style (16th Edition):

Shao, Qi. “Surface Signature of Flow Past a Sphere at Moderate Reynolds Numbers.” 2014. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/152601.

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

MLA Handbook (7th Edition):

Shao, Qi. “Surface Signature of Flow Past a Sphere at Moderate Reynolds Numbers.” 2014. Web. 21 Nov 2019.

Vancouver:

Shao Q. Surface Signature of Flow Past a Sphere at Moderate Reynolds Numbers. [Internet] [Thesis]. Texas A&M University; 2014. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/152601.

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

Council of Science Editors:

Shao Q. Surface Signature of Flow Past a Sphere at Moderate Reynolds Numbers. [Thesis]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/152601

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


Texas A&M University

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

Degree: 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. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/153665

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

Chicago Manual of Style (16th Edition):

Duncan, Jr., Glen T. “The Effects of Step Excrescences on Swept-Wing Boundary-Layer Transition.” 2014. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/153665.

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

MLA Handbook (7th Edition):

Duncan, Jr., Glen T. “The Effects of Step Excrescences on Swept-Wing Boundary-Layer Transition.” 2014. Web. 21 Nov 2019.

Vancouver:

Duncan, Jr. GT. The Effects of Step Excrescences on Swept-Wing Boundary-Layer Transition. [Internet] [Thesis]. Texas A&M University; 2014. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/153665.

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

Council of Science Editors:

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

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


Texas A&M University

10. Oliviero, Nick B. EPIC: A New and Advanced Nonlinear Parabolized Stability Equation Solver.

Degree: 2015, Texas A&M University

 Recent years have witnessed the linear and nonlinear parabolized stability equations (PSE) become a quintessential component toward understanding boundary-layer laminarto-turbulent transition. Because of the abundant… (more)

Subjects/Keywords: aerospace; hypersonic; boundary-layer transition; stability; parabolized stability equations; PSE; NPSE; LPSE

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APA (6th Edition):

Oliviero, N. B. (2015). EPIC: A New and Advanced Nonlinear Parabolized Stability Equation Solver. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/155252

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

Chicago Manual of Style (16th Edition):

Oliviero, Nick B. “EPIC: A New and Advanced Nonlinear Parabolized Stability Equation Solver.” 2015. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/155252.

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

MLA Handbook (7th Edition):

Oliviero, Nick B. “EPIC: A New and Advanced Nonlinear Parabolized Stability Equation Solver.” 2015. Web. 21 Nov 2019.

Vancouver:

Oliviero NB. EPIC: A New and Advanced Nonlinear Parabolized Stability Equation Solver. [Internet] [Thesis]. Texas A&M University; 2015. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/155252.

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

Council of Science Editors:

Oliviero NB. EPIC: A New and Advanced Nonlinear Parabolized Stability Equation Solver. [Thesis]. Texas A&M University; 2015. Available from: http://hdl.handle.net/1969.1/155252

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


Texas A&M University

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

Degree: 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. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/156395

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

Chicago Manual of Style (16th Edition):

Monschke, Jason Andrew. “Most-Critical Transient Disturbances in an Incompressible Flat-Plate Boundary Layer.” 2015. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/156395.

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

MLA Handbook (7th Edition):

Monschke, Jason Andrew. “Most-Critical Transient Disturbances in an Incompressible Flat-Plate Boundary Layer.” 2015. Web. 21 Nov 2019.

Vancouver:

Monschke JA. Most-Critical Transient Disturbances in an Incompressible Flat-Plate Boundary Layer. [Internet] [Thesis]. Texas A&M University; 2015. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/156395.

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

Council of Science Editors:

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

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


Texas A&M University

12. 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 November 21, 2019. 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. 21 Nov 2019.

Vancouver:

Kocian TS. Computational Hypersonic Boundary-Layer Stability and the Validation and Verification of EPIC. [Internet] [Doctoral dissertation]. Texas A&M University; 2018. [cited 2019 Nov 21]. 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

13. Buchanan, Kristopher Ryan. Theory and Applications of Aperiodic (Random) Phased Arrays.

Degree: 2014, Texas A&M University

 A need for network centric topologies using mobile wireless communications makes it important to investigate new distributed beamforming techniques. Platforms such as micro air vehicles… (more)

Subjects/Keywords: Random Array; Collaborative Beamforming; Opportunistic Array; Distributed Beamforming; Aperiodic Array; Spherical Random Antenna Array; Circular Random Antenna Array; Cooperative Systems

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APA (6th Edition):

Buchanan, K. R. (2014). Theory and Applications of Aperiodic (Random) Phased Arrays. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/157918

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

Chicago Manual of Style (16th Edition):

Buchanan, Kristopher Ryan. “Theory and Applications of Aperiodic (Random) Phased Arrays.” 2014. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/157918.

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

MLA Handbook (7th Edition):

Buchanan, Kristopher Ryan. “Theory and Applications of Aperiodic (Random) Phased Arrays.” 2014. Web. 21 Nov 2019.

Vancouver:

Buchanan KR. Theory and Applications of Aperiodic (Random) Phased Arrays. [Internet] [Thesis]. Texas A&M University; 2014. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/157918.

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

Council of Science Editors:

Buchanan KR. Theory and Applications of Aperiodic (Random) Phased Arrays. [Thesis]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/157918

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


Texas A&M University

14. Narang, Anshu. Analysis and Control of Non-Affine, Non-Standard, Singularly Perturbed Systems.

Degree: 2012, Texas A&M University

 This dissertation addresses the control problem for the general class of control non-affine, non-standard singularly perturbed continuous-time systems. The problem of control for nonlinear multiple… (more)

Subjects/Keywords: Tracking and regulation; Flight control; Non-Minimum phase systems; Singular perturbations; Multiple time scale; Nonlinear control theory

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APA (6th Edition):

Narang, A. (2012). Analysis and Control of Non-Affine, Non-Standard, Singularly Perturbed Systems. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/148104

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

Chicago Manual of Style (16th Edition):

Narang, Anshu. “Analysis and Control of Non-Affine, Non-Standard, Singularly Perturbed Systems.” 2012. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/148104.

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

MLA Handbook (7th Edition):

Narang, Anshu. “Analysis and Control of Non-Affine, Non-Standard, Singularly Perturbed Systems.” 2012. Web. 21 Nov 2019.

Vancouver:

Narang A. Analysis and Control of Non-Affine, Non-Standard, Singularly Perturbed Systems. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/148104.

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

Council of Science Editors:

Narang A. Analysis and Control of Non-Affine, Non-Standard, Singularly Perturbed Systems. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/148104

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


Texas A&M University

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

Degree: 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. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/151655

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

Chicago Manual of Style (16th Edition):

Belisle, Michael Joseph. “Aerodynamic Design for Swept-wing Laminar Flow.” 2013. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/151655.

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

MLA Handbook (7th Edition):

Belisle, Michael Joseph. “Aerodynamic Design for Swept-wing Laminar Flow.” 2013. Web. 21 Nov 2019.

Vancouver:

Belisle MJ. Aerodynamic Design for Swept-wing Laminar Flow. [Internet] [Thesis]. Texas A&M University; 2013. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/151655.

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

Council of Science Editors:

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

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


Texas A&M University

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

Degree: 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. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/152647

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

Chicago Manual of Style (16th Edition):

Sharp, Nicole Susanne. “Hypersonic Measurements of Roughness-Induced Transient Growth.” 2014. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/152647.

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

MLA Handbook (7th Edition):

Sharp, Nicole Susanne. “Hypersonic Measurements of Roughness-Induced Transient Growth.” 2014. Web. 21 Nov 2019.

Vancouver:

Sharp NS. Hypersonic Measurements of Roughness-Induced Transient Growth. [Internet] [Thesis]. Texas A&M University; 2014. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/152647.

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

Council of Science Editors:

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

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


Texas A&M University

17. Hafer, William Thomas. Sensitivity Methods Applied to Orbital Pursuit-Evasion.

Degree: 2014, Texas A&M University

 In this work, sensitivity methods are examined as a means to solve and analyze the problem of orbital pursuit-evasion (PE). Orbital PE is a two-sided… (more)

Subjects/Keywords: Orbital pursuit-evasion; sensitivity methods; barrier surfaces; two-sided optimal control

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APA (6th Edition):

Hafer, W. T. (2014). Sensitivity Methods Applied to Orbital Pursuit-Evasion. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/153412

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

Chicago Manual of Style (16th Edition):

Hafer, William Thomas. “Sensitivity Methods Applied to Orbital Pursuit-Evasion.” 2014. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/153412.

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

MLA Handbook (7th Edition):

Hafer, William Thomas. “Sensitivity Methods Applied to Orbital Pursuit-Evasion.” 2014. Web. 21 Nov 2019.

Vancouver:

Hafer WT. Sensitivity Methods Applied to Orbital Pursuit-Evasion. [Internet] [Thesis]. Texas A&M University; 2014. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/153412.

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

Council of Science Editors:

Hafer WT. Sensitivity Methods Applied to Orbital Pursuit-Evasion. [Thesis]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/153412

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


Texas A&M University

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

Degree: 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. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/154979

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

Chicago Manual of Style (16th Edition):

Crawford, Brian Keith. “Laminar-Turbulent Transition Due to 2-D Excrescences at 1% Chord on a Swept Wing.” 2015. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/154979.

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

MLA Handbook (7th Edition):

Crawford, Brian Keith. “Laminar-Turbulent Transition Due to 2-D Excrescences at 1% Chord on a Swept Wing.” 2015. Web. 21 Nov 2019.

Vancouver:

Crawford BK. Laminar-Turbulent Transition Due to 2-D Excrescences at 1% Chord on a Swept Wing. [Internet] [Thesis]. Texas A&M University; 2015. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/154979.

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

Council of Science Editors:

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

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


Texas A&M University

19. Pallampati, Sumana. Experimental Investigation of Origami Inspired Phased Arrays.

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

 Origami (the art of folding) can be incorporated into antenna systems to provide compact size and low weight designs. Apart from this, the system can… (more)

Subjects/Keywords: Phased Arrays; Origami; Reconfigurability; Ease of Deployment; Circular Patch; Circular Polarization; Miura Ori Fold; Impedance and Radiation Behavior

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APA (6th Edition):

Pallampati, S. (2017). Experimental Investigation of Origami Inspired Phased Arrays. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/165943

Chicago Manual of Style (16th Edition):

Pallampati, Sumana. “Experimental Investigation of Origami Inspired Phased Arrays.” 2017. Masters Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/165943.

MLA Handbook (7th Edition):

Pallampati, Sumana. “Experimental Investigation of Origami Inspired Phased Arrays.” 2017. Web. 21 Nov 2019.

Vancouver:

Pallampati S. Experimental Investigation of Origami Inspired Phased Arrays. [Internet] [Masters thesis]. Texas A&M University; 2017. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/165943.

Council of Science Editors:

Pallampati S. Experimental Investigation of Origami Inspired Phased Arrays. [Masters Thesis]. Texas A&M University; 2017. Available from: http://hdl.handle.net/1969.1/165943


Texas A&M University

20. Karimi, Mona. Compressibility Effects on the Kelvin-Helmholtz Instability and Mixing Layer Flows.

Degree: 2015, Texas A&M University

 The objective of the thesis is to analyze, understand and explicate the various physical mechanisms underlying the suppression of instability and mixing in compressible mixing… (more)

Subjects/Keywords: kelvin-Helmholtz instability; comressible mixing layers; shear flows; comressibility

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APA (6th Edition):

Karimi, M. (2015). Compressibility Effects on the Kelvin-Helmholtz Instability and Mixing Layer Flows. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/161262

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

Chicago Manual of Style (16th Edition):

Karimi, Mona. “Compressibility Effects on the Kelvin-Helmholtz Instability and Mixing Layer Flows.” 2015. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/161262.

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

MLA Handbook (7th Edition):

Karimi, Mona. “Compressibility Effects on the Kelvin-Helmholtz Instability and Mixing Layer Flows.” 2015. Web. 21 Nov 2019.

Vancouver:

Karimi M. Compressibility Effects on the Kelvin-Helmholtz Instability and Mixing Layer Flows. [Internet] [Thesis]. Texas A&M University; 2015. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/161262.

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

Council of Science Editors:

Karimi M. Compressibility Effects on the Kelvin-Helmholtz Instability and Mixing Layer Flows. [Thesis]. Texas A&M University; 2015. Available from: http://hdl.handle.net/1969.1/161262

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


Texas A&M University

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

Degree: 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. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/150990

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

Chicago Manual of Style (16th Edition):

Hofferth, Jerrod William. “Boundary-Layer Stability and Transition on a Flared Cone in a Mach 6 Quiet Wind Tunnel.” 2013. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/150990.

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

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. 21 Nov 2019.

Vancouver:

Hofferth JW. Boundary-Layer Stability and Transition on a Flared Cone in a Mach 6 Quiet Wind Tunnel. [Internet] [Thesis]. Texas A&M University; 2013. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/150990.

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

Council of Science Editors:

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

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

22. Roberts, Matthew William. Computational Evaluation of a Transonic Laminar-Flow Wing Glove Design.

Degree: 2012, Texas A&M University

 The aerodynamic benefits of laminar flow have long made it a sought-after attribute in aircraft design. By laminarizing portions of an aircraft, such as the… (more)

Subjects/Keywords: computational fluid dynamics; transonic; laminar flow; wing glove; boundary-layer stability; boundary-layer transition; laminar flow control; discrete roughness elements

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APA (6th Edition):

Roberts, M. W. (2012). Computational Evaluation of a Transonic Laminar-Flow Wing Glove Design. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10857

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

Chicago Manual of Style (16th Edition):

Roberts, Matthew William. “Computational Evaluation of a Transonic Laminar-Flow Wing Glove Design.” 2012. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10857.

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

MLA Handbook (7th Edition):

Roberts, Matthew William. “Computational Evaluation of a Transonic Laminar-Flow Wing Glove Design.” 2012. Web. 21 Nov 2019.

Vancouver:

Roberts MW. Computational Evaluation of a Transonic Laminar-Flow Wing Glove Design. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10857.

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

Council of Science Editors:

Roberts MW. Computational Evaluation of a Transonic Laminar-Flow Wing Glove Design. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10857

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

23. Hunt, Lauren Elizabeth. Boundary-Layer Receptivity to Three-Dimensional Roughness Arrays on a Swept-Wing.

Degree: 2012, Texas A&M University

 On-going efforts to reduce aircraft drag through transition delay focus on understanding the process of boundary-layer transition from a physics-based perspective. For swept-wings subject to… (more)

Subjects/Keywords: crossflow; boundary-layer transition

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APA (6th Edition):

Hunt, L. E. (2012). Boundary-Layer Receptivity to Three-Dimensional Roughness Arrays on a Swept-Wing. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10351

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

Chicago Manual of Style (16th Edition):

Hunt, Lauren Elizabeth. “Boundary-Layer Receptivity to Three-Dimensional Roughness Arrays on a Swept-Wing.” 2012. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10351.

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

MLA Handbook (7th Edition):

Hunt, Lauren Elizabeth. “Boundary-Layer Receptivity to Three-Dimensional Roughness Arrays on a Swept-Wing.” 2012. Web. 21 Nov 2019.

Vancouver:

Hunt LE. Boundary-Layer Receptivity to Three-Dimensional Roughness Arrays on a Swept-Wing. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10351.

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

Council of Science Editors:

Hunt LE. Boundary-Layer Receptivity to Three-Dimensional Roughness Arrays on a Swept-Wing. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10351

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

24. Taylor, David Christopher. The Characterization and Feasibility of a Low-Duty-Cycle Diaphragmless Shock Tube.

Degree: 2012, Texas A&M University

 The feasibility and characterization of a novel diaphragmless shock tube was examined at the National Aerothermochemistry Laboratory at Texas A&M University. The goal was to… (more)

Subjects/Keywords: Facility Development; Shock Tube; Aerospace Engineering

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APA (6th Edition):

Taylor, D. C. (2012). The Characterization and Feasibility of a Low-Duty-Cycle Diaphragmless Shock Tube. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11524

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

Chicago Manual of Style (16th Edition):

Taylor, David Christopher. “The Characterization and Feasibility of a Low-Duty-Cycle Diaphragmless Shock Tube.” 2012. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11524.

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

MLA Handbook (7th Edition):

Taylor, David Christopher. “The Characterization and Feasibility of a Low-Duty-Cycle Diaphragmless Shock Tube.” 2012. Web. 21 Nov 2019.

Vancouver:

Taylor DC. The Characterization and Feasibility of a Low-Duty-Cycle Diaphragmless Shock Tube. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11524.

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

Council of Science Editors:

Taylor DC. The Characterization and Feasibility of a Low-Duty-Cycle Diaphragmless Shock Tube. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11524

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

25. Goodnight, Ryan David. An Innovative Approach for Data Collection and Handling to Enable Advancements in Micro Air Vehicle Persistent Surveillance.

Degree: 2010, Texas A&M University

 The success of unmanned aerial vehicles (UAV) in the Iraq and Afghanistan conflicts has led to increased interest in further digitalization of the United States… (more)

Subjects/Keywords: MAV; Persistent Surveillance; Autonomous; Image Projection onto a terrain

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APA (6th Edition):

Goodnight, R. D. (2010). An Innovative Approach for Data Collection and Handling to Enable Advancements in Micro Air Vehicle Persistent Surveillance. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-7052

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

Chicago Manual of Style (16th Edition):

Goodnight, Ryan David. “An Innovative Approach for Data Collection and Handling to Enable Advancements in Micro Air Vehicle Persistent Surveillance.” 2010. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-7052.

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

MLA Handbook (7th Edition):

Goodnight, Ryan David. “An Innovative Approach for Data Collection and Handling to Enable Advancements in Micro Air Vehicle Persistent Surveillance.” 2010. Web. 21 Nov 2019.

Vancouver:

Goodnight RD. An Innovative Approach for Data Collection and Handling to Enable Advancements in Micro Air Vehicle Persistent Surveillance. [Internet] [Thesis]. Texas A&M University; 2010. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-7052.

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

Council of Science Editors:

Goodnight RD. An Innovative Approach for Data Collection and Handling to Enable Advancements in Micro Air Vehicle Persistent Surveillance. [Thesis]. Texas A&M University; 2010. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-7052

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

26. Neale, Tyler P. CFD Investigations of a Transonic Swept-Wing Laminar Flow Control Flight Experiment.

Degree: 2011, Texas A&M University

 Laminar flow control has been studied for several decades in an effort to achieve higher efficiencies for aircraft. Successful implementation of laminar flow control technology… (more)

Subjects/Keywords: Laminar flow control; crossflow; discrete roughness elements; aircraft CFD; turbofan simulation; airframe and turbofan integration

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APA (6th Edition):

Neale, T. P. (2011). CFD Investigations of a Transonic Swept-Wing Laminar Flow Control Flight Experiment. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-7889

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

Chicago Manual of Style (16th Edition):

Neale, Tyler P. “CFD Investigations of a Transonic Swept-Wing Laminar Flow Control Flight Experiment.” 2011. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-7889.

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

MLA Handbook (7th Edition):

Neale, Tyler P. “CFD Investigations of a Transonic Swept-Wing Laminar Flow Control Flight Experiment.” 2011. Web. 21 Nov 2019.

Vancouver:

Neale TP. CFD Investigations of a Transonic Swept-Wing Laminar Flow Control Flight Experiment. [Internet] [Thesis]. Texas A&M University; 2011. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-7889.

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

Council of Science Editors:

Neale TP. CFD Investigations of a Transonic Swept-Wing Laminar Flow Control Flight Experiment. [Thesis]. Texas A&M University; 2011. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-7889

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

27. Williams, Thomas 1987-. Design of an Instrumentation System for a Boundary Layer Transition Wing Glove Experiment.

Degree: 2012, Texas A&M University

 Laminar flow control holds major promise for increasing aircraft efficiency and increasing laminar flow over aerodynamic surfaces could decrease drag by up to 30 percent.… (more)

Subjects/Keywords: traveling wave; heat transfer; boundary layer transition; boundary layer; transition; hotfilms; wing glove; laminar flow

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APA (6th Edition):

Williams, T. 1. (2012). Design of an Instrumentation System for a Boundary Layer Transition Wing Glove Experiment. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/148348

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

Chicago Manual of Style (16th Edition):

Williams, Thomas 1987-. “Design of an Instrumentation System for a Boundary Layer Transition Wing Glove Experiment.” 2012. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/148348.

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

MLA Handbook (7th Edition):

Williams, Thomas 1987-. “Design of an Instrumentation System for a Boundary Layer Transition Wing Glove Experiment.” 2012. Web. 21 Nov 2019.

Vancouver:

Williams T1. Design of an Instrumentation System for a Boundary Layer Transition Wing Glove Experiment. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/148348.

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

Council of Science Editors:

Williams T1. Design of an Instrumentation System for a Boundary Layer Transition Wing Glove Experiment. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/148348

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

28. Finn, Thomas Patrick. Experimental Study and Computational Turbulence Modeling of Combined Rayleigh-Taylor and Kelvin-Helmholtz Mixing with Complex Stratification.

Degree: 2014, Texas A&M University

 An experimental study of the combined Rayleigh-Taylor instability (RTI) and Kelvin-Helmholtz instability (KHI) is presented at three different Atwood numbers (0.05, 0.971, 0.147) and multiple… (more)

Subjects/Keywords: Rayleigh-Taylor Instability; Kelvin-Helmholtz Instability; Complex Stratification; Reynolds-Averaged Navier-Stokes Model; Multilayer Gas Tunnel Facility

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APA (6th Edition):

Finn, T. P. (2014). Experimental Study and Computational Turbulence Modeling of Combined Rayleigh-Taylor and Kelvin-Helmholtz Mixing with Complex Stratification. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/153312

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

Chicago Manual of Style (16th Edition):

Finn, Thomas Patrick. “Experimental Study and Computational Turbulence Modeling of Combined Rayleigh-Taylor and Kelvin-Helmholtz Mixing with Complex Stratification.” 2014. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/153312.

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

MLA Handbook (7th Edition):

Finn, Thomas Patrick. “Experimental Study and Computational Turbulence Modeling of Combined Rayleigh-Taylor and Kelvin-Helmholtz Mixing with Complex Stratification.” 2014. Web. 21 Nov 2019.

Vancouver:

Finn TP. Experimental Study and Computational Turbulence Modeling of Combined Rayleigh-Taylor and Kelvin-Helmholtz Mixing with Complex Stratification. [Internet] [Thesis]. Texas A&M University; 2014. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/153312.

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

Council of Science Editors:

Finn TP. Experimental Study and Computational Turbulence Modeling of Combined Rayleigh-Taylor and Kelvin-Helmholtz Mixing with Complex Stratification. [Thesis]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/153312

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

29. West, David Edward. Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements.

Degree: 2014, Texas A&M University

 Micron-sized, spanwise-periodic, discrete roughness elements (DREs) were applied to and tested on a 30? swept-wing model in order to study their effects on boundary-layer transition… (more)

Subjects/Keywords: discrete roughness elements; DRE; laminar flow control; transition; laminar-turbulent; experiment; flight; swept wing; sensitivity; spanwise-periodic; Texas A&M; Flight Research Lab

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

APA (6th Edition):

West, D. E. (2014). Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/154330

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

Chicago Manual of Style (16th Edition):

West, David Edward. “Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements.” 2014. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/154330.

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

MLA Handbook (7th Edition):

West, David Edward. “Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements.” 2014. Web. 21 Nov 2019.

Vancouver:

West DE. Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements. [Internet] [Thesis]. Texas A&M University; 2014. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/154330.

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

Council of Science Editors:

West DE. Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements. [Thesis]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/154330

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

30. West, David Edward. Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements.

Degree: 2014, Texas A&M University

 Micron-sized, spanwise-periodic, discrete roughness elements (DREs) were applied to and tested on a 30? swept-wing model in order to study their effects on boundary-layer transition… (more)

Subjects/Keywords: discrete roughness elements; DRE; laminar flow control; transition; laminar-turbulent; experiment; flight; swept wing; sensitivity; spanwise-periodic; Texas A&M; Flight Research Lab

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

West, D. E. (2014). Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/154230

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

Chicago Manual of Style (16th Edition):

West, David Edward. “Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements.” 2014. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/154230.

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

MLA Handbook (7th Edition):

West, David Edward. “Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements.” 2014. Web. 21 Nov 2019.

Vancouver:

West DE. Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements. [Internet] [Thesis]. Texas A&M University; 2014. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/154230.

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

Council of Science Editors:

West DE. Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements. [Thesis]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/154230

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

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