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You searched for +publisher:"Texas A&M University" +contributor:("Saric, William S"). Showing records 1 – 19 of 19 total matches.

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Texas A&M University

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

Degree: 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. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10731

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):

Kuester, Matthew. “Acoustics in the Klebanoff-Saric Wind Tunnel: Background Identification, Forcing, and Active Control.” 2012. Thesis, Texas A&M University. Accessed December 08, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10731.

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

MLA Handbook (7th Edition):

Kuester, Matthew. “Acoustics in the Klebanoff-Saric Wind Tunnel: Background Identification, Forcing, and Active Control.” 2012. Web. 08 Dec 2019.

Vancouver:

Kuester M. Acoustics in the Klebanoff-Saric Wind Tunnel: Background Identification, Forcing, and Active Control. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10731.

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

Council of Science Editors:

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

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


Texas A&M University

2. Schouten, Shane Michael. Complete CFD analysis of a Velocity XL-5 RG with flight-test verification.

Degree: 2008, Texas A&M University

 The Texas A&M Flight Research Laboratory (FRL) recently received delivery of its newest aircraft, the Velocity XL-5 RG. The Velocity can fly faster than the… (more)

Subjects/Keywords: CFD; flight-test; wind tunnel tests; Cimcore Coordinate Measurement Machine; Velocity XL-5 RG

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APA (6th Edition):

Schouten, S. M. (2008). Complete CFD analysis of a Velocity XL-5 RG with flight-test verification. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/85894

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):

Schouten, Shane Michael. “Complete CFD analysis of a Velocity XL-5 RG with flight-test verification.” 2008. Thesis, Texas A&M University. Accessed December 08, 2019. http://hdl.handle.net/1969.1/85894.

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

MLA Handbook (7th Edition):

Schouten, Shane Michael. “Complete CFD analysis of a Velocity XL-5 RG with flight-test verification.” 2008. Web. 08 Dec 2019.

Vancouver:

Schouten SM. Complete CFD analysis of a Velocity XL-5 RG with flight-test verification. [Internet] [Thesis]. Texas A&M University; 2008. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/1969.1/85894.

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

Council of Science Editors:

Schouten SM. Complete CFD analysis of a Velocity XL-5 RG with flight-test verification. [Thesis]. Texas A&M University; 2008. Available from: http://hdl.handle.net/1969.1/85894

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


Texas A&M University

3. Mishra, Aashwin A. A Dynamical Systems Approach Towards Modeling the Rapid Pressure Strain Correlation.

Degree: 2011, Texas A&M University

 In this study, the behavior of pressure in the Rapid Distortion Limit, along with its concomitant modeling, are addressed. In the first part of the… (more)

Subjects/Keywords: Fluid mechanics; Turbulence modeling; second moment closures; pressure strain correlation; rapid distortion theory; dynamical systems

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APA (6th Edition):

Mishra, A. A. (2011). A Dynamical Systems Approach Towards Modeling the Rapid Pressure Strain Correlation. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8018

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):

Mishra, Aashwin A. “A Dynamical Systems Approach Towards Modeling the Rapid Pressure Strain Correlation.” 2011. Thesis, Texas A&M University. Accessed December 08, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8018.

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

MLA Handbook (7th Edition):

Mishra, Aashwin A. “A Dynamical Systems Approach Towards Modeling the Rapid Pressure Strain Correlation.” 2011. Web. 08 Dec 2019.

Vancouver:

Mishra AA. A Dynamical Systems Approach Towards Modeling the Rapid Pressure Strain Correlation. [Internet] [Thesis]. Texas A&M University; 2011. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8018.

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

Council of Science Editors:

Mishra AA. A Dynamical Systems Approach Towards Modeling the Rapid Pressure Strain Correlation. [Thesis]. Texas A&M University; 2011. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8018

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


Texas A&M University

4. Tahvildari, Navid. Nonlinear Interactions between Longs Waves in a Two-Layer Fluid.

Degree: 2012, Texas A&M University

 The nonlinear interactions between long surface waves and interfacial waves in a two-layer fluid are studied theoretically. The fluid is density-stratified and the thicknesses of… (more)

Subjects/Keywords: Interfacial waves; Surface waves; Nonlinear interactions; Boussinesq equation

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APA (6th Edition):

Tahvildari, N. (2012). Nonlinear Interactions between Longs Waves in a Two-Layer Fluid. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10556

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):

Tahvildari, Navid. “Nonlinear Interactions between Longs Waves in a Two-Layer Fluid.” 2012. Thesis, Texas A&M University. Accessed December 08, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10556.

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

MLA Handbook (7th Edition):

Tahvildari, Navid. “Nonlinear Interactions between Longs Waves in a Two-Layer Fluid.” 2012. Web. 08 Dec 2019.

Vancouver:

Tahvildari N. Nonlinear Interactions between Longs Waves in a Two-Layer Fluid. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10556.

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

Council of Science Editors:

Tahvildari N. Nonlinear Interactions between Longs Waves in a Two-Layer Fluid. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10556

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


Texas A&M University

5. 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 December 08, 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. 08 Dec 2019.

Vancouver:

Belisle MJ. Aerodynamic Design for Swept-wing Laminar Flow. [Internet] [Thesis]. Texas A&M University; 2013. [cited 2019 Dec 08]. 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

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

Degree: 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. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/152606

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):

Kuester, Matthew Scott. “Distributed Roughness Receptivity in a Flat Plate Boundary Layer.” 2014. Thesis, Texas A&M University. Accessed December 08, 2019. http://hdl.handle.net/1969.1/152606.

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

MLA Handbook (7th Edition):

Kuester, Matthew Scott. “Distributed Roughness Receptivity in a Flat Plate Boundary Layer.” 2014. Web. 08 Dec 2019.

Vancouver:

Kuester MS. Distributed Roughness Receptivity in a Flat Plate Boundary Layer. [Internet] [Thesis]. Texas A&M University; 2014. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/1969.1/152606.

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

Council of Science Editors:

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

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


Texas A&M University

7. 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 December 08, 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. 08 Dec 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 Dec 08]. 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

8. 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 December 08, 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. 08 Dec 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 Dec 08]. 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

9. 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 December 08, 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. 08 Dec 2019.

Vancouver:

Roberts MW. Computational Evaluation of a Transonic Laminar-Flow Wing Glove Design. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Dec 08]. 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

10. 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 December 08, 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. 08 Dec 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 Dec 08]. 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

11. 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 December 08, 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. 08 Dec 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 Dec 08]. 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

12. 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 (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 December 08, 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. 08 Dec 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 Dec 08]. 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

13. 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/1969.1/154230

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 December 08, 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. 08 Dec 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 Dec 08]. 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

14. Carpenter, Andrew L. In-flight Receptivity Experiments on a 30-degree Swept-wing using Micron-sized Discrete Roughness Elements.

Degree: 2010, Texas A&M University

 One of the last remaining challenges preventing the laminarization of sweptwings is the control of unstable crossflow vortices. In low-disturbance environments the transition from laminar… (more)

Subjects/Keywords: Receptivity; Laminar Flow; Boundary Layer; Swept-Wing; Roughness; Hotfilms; Infrared Thermography; Flight Test

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APA (6th Edition):

Carpenter, A. L. (2010). In-flight Receptivity Experiments on a 30-degree Swept-wing using Micron-sized Discrete Roughness Elements. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2009-05-728

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):

Carpenter, Andrew L. “In-flight Receptivity Experiments on a 30-degree Swept-wing using Micron-sized Discrete Roughness Elements.” 2010. Thesis, Texas A&M University. Accessed December 08, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2009-05-728.

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

MLA Handbook (7th Edition):

Carpenter, Andrew L. “In-flight Receptivity Experiments on a 30-degree Swept-wing using Micron-sized Discrete Roughness Elements.” 2010. Web. 08 Dec 2019.

Vancouver:

Carpenter AL. In-flight Receptivity Experiments on a 30-degree Swept-wing using Micron-sized Discrete Roughness Elements. [Internet] [Thesis]. Texas A&M University; 2010. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-05-728.

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

Council of Science Editors:

Carpenter AL. In-flight Receptivity Experiments on a 30-degree Swept-wing using Micron-sized Discrete Roughness Elements. [Thesis]. Texas A&M University; 2010. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-05-728

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

15. Hedderman, Simon Peter. Developments for a Swept Wing Airfoil to Study the Effects of Step and Gap Excrescences on Boundary Layer Transition.

Degree: 2013, Texas A&M University

 Skin friction drag reduction is one of the most promising paths in the investigation of the reduction of aircraft fuel burn. 40 ? 50% of… (more)

Subjects/Keywords: boundary layer; stability; excrescence; excrescences; SWIFT; SWIFTER; step; gap; airfoil; swept wing; actuation control system; heating sheet; wind tunnel; wall liners; natural laminar flow; nlf

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APA (6th Edition):

Hedderman, S. P. (2013). Developments for a Swept Wing Airfoil to Study the Effects of Step and Gap Excrescences on Boundary Layer Transition. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/149269

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):

Hedderman, Simon Peter. “Developments for a Swept Wing Airfoil to Study the Effects of Step and Gap Excrescences on Boundary Layer Transition.” 2013. Thesis, Texas A&M University. Accessed December 08, 2019. http://hdl.handle.net/1969.1/149269.

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

MLA Handbook (7th Edition):

Hedderman, Simon Peter. “Developments for a Swept Wing Airfoil to Study the Effects of Step and Gap Excrescences on Boundary Layer Transition.” 2013. Web. 08 Dec 2019.

Vancouver:

Hedderman SP. Developments for a Swept Wing Airfoil to Study the Effects of Step and Gap Excrescences on Boundary Layer Transition. [Internet] [Thesis]. Texas A&M University; 2013. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/1969.1/149269.

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

Council of Science Editors:

Hedderman SP. Developments for a Swept Wing Airfoil to Study the Effects of Step and Gap Excrescences on Boundary Layer Transition. [Thesis]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/149269

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

16. Tufts, Matthew W. Computational Investigation of Sensitivity of the Crossflow Instability to Two-Dimensional Surface Imperfections.

Degree: 2015, Texas A&M University

 The interaction between two-dimensional steps and gaps with stationary cross?ow vortices on a swept laminar wing has been investigated using computational methods. Using ?ow conditions… (more)

Subjects/Keywords: Laminar Flow; Transition; Swept-Wing

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

APA (6th Edition):

Tufts, M. W. (2015). Computational Investigation of Sensitivity of the Crossflow Instability to Two-Dimensional Surface Imperfections. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/156386

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):

Tufts, Matthew W. “Computational Investigation of Sensitivity of the Crossflow Instability to Two-Dimensional Surface Imperfections.” 2015. Thesis, Texas A&M University. Accessed December 08, 2019. http://hdl.handle.net/1969.1/156386.

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

MLA Handbook (7th Edition):

Tufts, Matthew W. “Computational Investigation of Sensitivity of the Crossflow Instability to Two-Dimensional Surface Imperfections.” 2015. Web. 08 Dec 2019.

Vancouver:

Tufts MW. Computational Investigation of Sensitivity of the Crossflow Instability to Two-Dimensional Surface Imperfections. [Internet] [Thesis]. Texas A&M University; 2015. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/1969.1/156386.

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

Council of Science Editors:

Tufts MW. Computational Investigation of Sensitivity of the Crossflow Instability to Two-Dimensional Surface Imperfections. [Thesis]. Texas A&M University; 2015. Available from: http://hdl.handle.net/1969.1/156386

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

17. Tucker, Aaron 1975-. Laminar Flow Control Flight Experiment Design.

Degree: 2012, Texas A&M University

 Demonstration of spanwise-periodic discrete roughness element laminar flow control (DRE LFC) technology at operationally relevant flight regimes requires extremely stable flow conditions in flight. A… (more)

Subjects/Keywords: design of experiments; wing glove; flight test technique; flight test; flight research; laminar flow control

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

APA (6th Edition):

Tucker, A. 1. (2012). Laminar Flow Control Flight Experiment Design. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/148399

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):

Tucker, Aaron 1975-. “Laminar Flow Control Flight Experiment Design.” 2012. Thesis, Texas A&M University. Accessed December 08, 2019. http://hdl.handle.net/1969.1/148399.

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

MLA Handbook (7th Edition):

Tucker, Aaron 1975-. “Laminar Flow Control Flight Experiment Design.” 2012. Web. 08 Dec 2019.

Vancouver:

Tucker A1. Laminar Flow Control Flight Experiment Design. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/1969.1/148399.

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

Council of Science Editors:

Tucker A1. Laminar Flow Control Flight Experiment Design. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/148399

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

18. Craig, Stuart A. Stability of High-Speed, Three-Dimensional Boundary Layers.

Degree: 2015, Texas A&M University

 Boundary-layer experiments are performed in the low-disturbance, Mach 6 Quiet Tunnel (M6QT) at Texas A&M University. The experiments are focused specifically on investigating the physics… (more)

Subjects/Keywords: boundary layers; laminar-turbulent transition; crossflow; hypersonics; fluid mechanics; aerodynamics

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

APA (6th Edition):

Craig, S. A. (2015). Stability of High-Speed, Three-Dimensional Boundary Layers. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/155069

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):

Craig, Stuart A. “Stability of High-Speed, Three-Dimensional Boundary Layers.” 2015. Thesis, Texas A&M University. Accessed December 08, 2019. http://hdl.handle.net/1969.1/155069.

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

MLA Handbook (7th Edition):

Craig, Stuart A. “Stability of High-Speed, Three-Dimensional Boundary Layers.” 2015. Web. 08 Dec 2019.

Vancouver:

Craig SA. Stability of High-Speed, Three-Dimensional Boundary Layers. [Internet] [Thesis]. Texas A&M University; 2015. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/1969.1/155069.

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

Council of Science Editors:

Craig SA. Stability of High-Speed, Three-Dimensional Boundary Layers. [Thesis]. Texas A&M University; 2015. Available from: http://hdl.handle.net/1969.1/155069

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


Texas A&M University

19. McKnight, Christopher William. Design and safety analysis of an in-flight, test airfoil.

Degree: 2006, Texas A&M University

 The evaluation of an in-flight airfoil model requires extensive analysis of a variety of structural systems. Determining the safety of the design is a unique… (more)

Subjects/Keywords: Aerospace Design; Flight Testing

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

APA (6th Edition):

McKnight, C. W. (2006). Design and safety analysis of an in-flight, test airfoil. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/4398

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):

McKnight, Christopher William. “Design and safety analysis of an in-flight, test airfoil.” 2006. Thesis, Texas A&M University. Accessed December 08, 2019. http://hdl.handle.net/1969.1/4398.

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

MLA Handbook (7th Edition):

McKnight, Christopher William. “Design and safety analysis of an in-flight, test airfoil.” 2006. Web. 08 Dec 2019.

Vancouver:

McKnight CW. Design and safety analysis of an in-flight, test airfoil. [Internet] [Thesis]. Texas A&M University; 2006. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/1969.1/4398.

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

Council of Science Editors:

McKnight CW. Design and safety analysis of an in-flight, test airfoil. [Thesis]. Texas A&M University; 2006. Available from: http://hdl.handle.net/1969.1/4398

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

.