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You searched for +publisher:"Texas A&M University" +contributor:("Cizmas, Paul"). Showing records 1 – 30 of 55 total matches.

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Texas A&M University

1. Thorat, Manish R. Impact of Rotor Surface Velocity, Leakage Models and Real Gas Properties on Rotordynamic Force Predictions of Gas Labyrinth Seals.

Degree: 2010, Texas A&M University

 Rotordynamic coefficients of a gas labyrinth seal are assumed to be frequency independent. However, this assumption loses its validity as rotor surface velocity approaches Mach… (more)

Subjects/Keywords: Labyrinth Seal; Rotordynamics

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

APA (6th Edition):

Thorat, M. R. (2010). Impact of Rotor Surface Velocity, Leakage Models and Real Gas Properties on Rotordynamic Force Predictions of Gas Labyrinth Seals. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-7861

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):

Thorat, Manish R. “Impact of Rotor Surface Velocity, Leakage Models and Real Gas Properties on Rotordynamic Force Predictions of Gas Labyrinth Seals.” 2010. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-7861.

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

MLA Handbook (7th Edition):

Thorat, Manish R. “Impact of Rotor Surface Velocity, Leakage Models and Real Gas Properties on Rotordynamic Force Predictions of Gas Labyrinth Seals.” 2010. Web. 18 Oct 2019.

Vancouver:

Thorat MR. Impact of Rotor Surface Velocity, Leakage Models and Real Gas Properties on Rotordynamic Force Predictions of Gas Labyrinth Seals. [Internet] [Thesis]. Texas A&M University; 2010. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-7861.

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

Council of Science Editors:

Thorat MR. Impact of Rotor Surface Velocity, Leakage Models and Real Gas Properties on Rotordynamic Force Predictions of Gas Labyrinth Seals. [Thesis]. Texas A&M University; 2010. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-7861

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


Texas A&M University

2. Deva Asirvatham, Thanesh. Friction Factor Measurement, Analysis, and Modeling for Flat-Plates with 12.15 mm Diameter Hole-Pattern, Tested with Air at Different Clearances, Inlet Pressures, and Pressure Ratios.

Degree: 2011, Texas A&M University

 Friction factor data are important for better prediction of leakage and rotordynamic coefficients of gas annular seals. A flat-plate test rig is used to determine… (more)

Subjects/Keywords: Flat plate testing; Friction factor; Gas annular seal

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APA (6th Edition):

Deva Asirvatham, T. (2011). Friction Factor Measurement, Analysis, and Modeling for Flat-Plates with 12.15 mm Diameter Hole-Pattern, Tested with Air at Different Clearances, Inlet Pressures, and Pressure Ratios. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-12-8970

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):

Deva Asirvatham, Thanesh. “Friction Factor Measurement, Analysis, and Modeling for Flat-Plates with 12.15 mm Diameter Hole-Pattern, Tested with Air at Different Clearances, Inlet Pressures, and Pressure Ratios.” 2011. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2010-12-8970.

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

MLA Handbook (7th Edition):

Deva Asirvatham, Thanesh. “Friction Factor Measurement, Analysis, and Modeling for Flat-Plates with 12.15 mm Diameter Hole-Pattern, Tested with Air at Different Clearances, Inlet Pressures, and Pressure Ratios.” 2011. Web. 18 Oct 2019.

Vancouver:

Deva Asirvatham T. Friction Factor Measurement, Analysis, and Modeling for Flat-Plates with 12.15 mm Diameter Hole-Pattern, Tested with Air at Different Clearances, Inlet Pressures, and Pressure Ratios. [Internet] [Thesis]. Texas A&M University; 2011. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-12-8970.

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

Council of Science Editors:

Deva Asirvatham T. Friction Factor Measurement, Analysis, and Modeling for Flat-Plates with 12.15 mm Diameter Hole-Pattern, Tested with Air at Different Clearances, Inlet Pressures, and Pressure Ratios. [Thesis]. Texas A&M University; 2011. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-12-8970

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


Texas A&M University

3. Appel, Bradley. Multiphysics Design and Simulation of a Tungsten-Cermet Nuclear Thermal Rocket.

Degree: 2012, Texas A&M University

 The goal of this research is to apply modern methods of analysis to the design of a tungsten-cermet Nuclear Thermal Rocket (NTR) core. An NTR… (more)

Subjects/Keywords: nuclear; rocket; CFD; propulsion

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APA (6th Edition):

Appel, B. (2012). Multiphysics Design and Simulation of a Tungsten-Cermet Nuclear Thermal Rocket. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11649

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):

Appel, Bradley. “Multiphysics Design and Simulation of a Tungsten-Cermet Nuclear Thermal Rocket.” 2012. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11649.

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

MLA Handbook (7th Edition):

Appel, Bradley. “Multiphysics Design and Simulation of a Tungsten-Cermet Nuclear Thermal Rocket.” 2012. Web. 18 Oct 2019.

Vancouver:

Appel B. Multiphysics Design and Simulation of a Tungsten-Cermet Nuclear Thermal Rocket. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11649.

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

Council of Science Editors:

Appel B. Multiphysics Design and Simulation of a Tungsten-Cermet Nuclear Thermal Rocket. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11649

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


Texas A&M University

4. Greer, Christopher Alden. Simulation of Creep in Micron Scale Crystalline Materials for High Temperature Thermal Protection Systems.

Degree: 2016, Texas A&M University

 The use of thermal barrier coatings over the past few decades has signi?cantly improved the performance of gas turbine engines by reducing the operating temper-ature… (more)

Subjects/Keywords: Creep; Dislocation Dynamics

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APA (6th Edition):

Greer, C. A. (2016). Simulation of Creep in Micron Scale Crystalline Materials for High Temperature Thermal Protection Systems. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/157146

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):

Greer, Christopher Alden. “Simulation of Creep in Micron Scale Crystalline Materials for High Temperature Thermal Protection Systems.” 2016. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/157146.

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

MLA Handbook (7th Edition):

Greer, Christopher Alden. “Simulation of Creep in Micron Scale Crystalline Materials for High Temperature Thermal Protection Systems.” 2016. Web. 18 Oct 2019.

Vancouver:

Greer CA. Simulation of Creep in Micron Scale Crystalline Materials for High Temperature Thermal Protection Systems. [Internet] [Thesis]. Texas A&M University; 2016. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/157146.

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

Council of Science Editors:

Greer CA. Simulation of Creep in Micron Scale Crystalline Materials for High Temperature Thermal Protection Systems. [Thesis]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/157146

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


Texas A&M University

5. Richardson, Brian Ross. A reduced-order model based on proper orthogonal decomposition for non-isothermal two-phase flows.

Degree: 2009, Texas A&M University

 This thesis presents a study of reduced-order models based on proper orthogonal decomposition applied to non-isothermal transport phenomena in ?uidized beds. A numerical ?ow solver… (more)

Subjects/Keywords: Proper Orthogonal Decomposition; Reduced-Order Model; Numerical Methods

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APA (6th Edition):

Richardson, B. R. (2009). A reduced-order model based on proper orthogonal decomposition for non-isothermal two-phase flows. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2623

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):

Richardson, Brian Ross. “A reduced-order model based on proper orthogonal decomposition for non-isothermal two-phase flows.” 2009. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2623.

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

MLA Handbook (7th Edition):

Richardson, Brian Ross. “A reduced-order model based on proper orthogonal decomposition for non-isothermal two-phase flows.” 2009. Web. 18 Oct 2019.

Vancouver:

Richardson BR. A reduced-order model based on proper orthogonal decomposition for non-isothermal two-phase flows. [Internet] [Thesis]. Texas A&M University; 2009. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2623.

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

Council of Science Editors:

Richardson BR. A reduced-order model based on proper orthogonal decomposition for non-isothermal two-phase flows. [Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2623

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


Texas A&M University

6. Stephens, Matthew Aaron. Tailoring the plateau burning rates of composite propellants by the use of nanoscale additives.

Degree: 2009, Texas A&M University

 Composite propellants are composed of a solid oxidizer that is mixed into a hydrocarbon binder that when polymerized results in a solid mass capable of… (more)

Subjects/Keywords: Solid Propellant; Nanoparticles

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APA (6th Edition):

Stephens, M. A. (2009). Tailoring the plateau burning rates of composite propellants by the use of nanoscale additives. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-3202

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):

Stephens, Matthew Aaron. “Tailoring the plateau burning rates of composite propellants by the use of nanoscale additives.” 2009. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-3202.

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

MLA Handbook (7th Edition):

Stephens, Matthew Aaron. “Tailoring the plateau burning rates of composite propellants by the use of nanoscale additives.” 2009. Web. 18 Oct 2019.

Vancouver:

Stephens MA. Tailoring the plateau burning rates of composite propellants by the use of nanoscale additives. [Internet] [Thesis]. Texas A&M University; 2009. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-3202.

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

Council of Science Editors:

Stephens MA. Tailoring the plateau burning rates of composite propellants by the use of nanoscale additives. [Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-3202

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


Texas A&M University

7. Wilkes, Jason C. A PERSPECTIVE ON THE NUMERICAL AND EXPERIMENTAL CHARACTERISTICS OF MULTI-MODE DRY-FRICTION WHIP AND WHIRL.

Degree: 2010, Texas A&M University

 The present work investigates the nature of dry-friction whip and whirl through experimental and numerical methods. Efforts of the author, Dyck, Pavalek, and coworkers enabled… (more)

Subjects/Keywords: rotordynamics; whirl; whip; rub; rotor; stator; contact

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APA (6th Edition):

Wilkes, J. C. (2010). A PERSPECTIVE ON THE NUMERICAL AND EXPERIMENTAL CHARACTERISTICS OF MULTI-MODE DRY-FRICTION WHIP AND WHIRL. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2008-08-44

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):

Wilkes, Jason C. “A PERSPECTIVE ON THE NUMERICAL AND EXPERIMENTAL CHARACTERISTICS OF MULTI-MODE DRY-FRICTION WHIP AND WHIRL.” 2010. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2008-08-44.

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

MLA Handbook (7th Edition):

Wilkes, Jason C. “A PERSPECTIVE ON THE NUMERICAL AND EXPERIMENTAL CHARACTERISTICS OF MULTI-MODE DRY-FRICTION WHIP AND WHIRL.” 2010. Web. 18 Oct 2019.

Vancouver:

Wilkes JC. A PERSPECTIVE ON THE NUMERICAL AND EXPERIMENTAL CHARACTERISTICS OF MULTI-MODE DRY-FRICTION WHIP AND WHIRL. [Internet] [Thesis]. Texas A&M University; 2010. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2008-08-44.

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

Council of Science Editors:

Wilkes JC. A PERSPECTIVE ON THE NUMERICAL AND EXPERIMENTAL CHARACTERISTICS OF MULTI-MODE DRY-FRICTION WHIP AND WHIRL. [Thesis]. Texas A&M University; 2010. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2008-08-44

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


Texas A&M University

8. Worley, Gregory. A Conformal Mapping Grid Generation Method for Modeling High-Fidelity Aeroelastic Simulations.

Degree: 2010, Texas A&M University

 This work presents a method for building a three-dimensional mesh from two- dimensional topologically identical layers, for use in aeroelastic simulations. The method allows modeling… (more)

Subjects/Keywords: Aeroelasticity; unsteady aerodynamics; computational fl uid dynamics; grid generation; conformal mapping; limit cycle oscillation; nonlinear

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APA (6th Edition):

Worley, G. (2010). A Conformal Mapping Grid Generation Method for Modeling High-Fidelity Aeroelastic Simulations. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-7747

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):

Worley, Gregory. “A Conformal Mapping Grid Generation Method for Modeling High-Fidelity Aeroelastic Simulations.” 2010. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-7747.

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

MLA Handbook (7th Edition):

Worley, Gregory. “A Conformal Mapping Grid Generation Method for Modeling High-Fidelity Aeroelastic Simulations.” 2010. Web. 18 Oct 2019.

Vancouver:

Worley G. A Conformal Mapping Grid Generation Method for Modeling High-Fidelity Aeroelastic Simulations. [Internet] [Thesis]. Texas A&M University; 2010. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-7747.

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

Council of Science Editors:

Worley G. A Conformal Mapping Grid Generation Method for Modeling High-Fidelity Aeroelastic Simulations. [Thesis]. Texas A&M University; 2010. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-7747

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


Texas A&M University

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

Degree: 2011, Texas A&M University

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

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

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APA (6th Edition):

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

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):

Johnson, Shalom. “Development of a Pulse Modulator for Active Flow Control in Turbomachinery.” 2011. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8035.

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

MLA Handbook (7th Edition):

Johnson, Shalom. “Development of a Pulse Modulator for Active Flow Control in Turbomachinery.” 2011. Web. 18 Oct 2019.

Vancouver:

Johnson S. Development of a Pulse Modulator for Active Flow Control in Turbomachinery. [Internet] [Thesis]. Texas A&M University; 2011. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8035.

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

Council of Science Editors:

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

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


Texas A&M University

10. Mehta, Naitik. Comparison of a Slanted-Tooth See-Through Labyrinth Seal to a Straight-Tooth See-Through Labyrinth Seal for Rotordynamic Coefficients and Leakage.

Degree: 2012, Texas A&M University

 This research compares the leakage and rotordynamic characteristics of a slanted-tooth labyrinth seal to a conventional straight-tooth labyrinth. Detailed results comparing the rotordynamic coefficients and… (more)

Subjects/Keywords: Labyrinth Seal; Rotordynamic; Stiffness; Damping; Leakage; Slant; Straight; Inclined; Slanted-Tooth; Straight-Tooth

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APA (6th Edition):

Mehta, N. (2012). Comparison of a Slanted-Tooth See-Through Labyrinth Seal to a Straight-Tooth See-Through Labyrinth Seal for Rotordynamic Coefficients and Leakage. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10825

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):

Mehta, Naitik. “Comparison of a Slanted-Tooth See-Through Labyrinth Seal to a Straight-Tooth See-Through Labyrinth Seal for Rotordynamic Coefficients and Leakage.” 2012. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10825.

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

MLA Handbook (7th Edition):

Mehta, Naitik. “Comparison of a Slanted-Tooth See-Through Labyrinth Seal to a Straight-Tooth See-Through Labyrinth Seal for Rotordynamic Coefficients and Leakage.” 2012. Web. 18 Oct 2019.

Vancouver:

Mehta N. Comparison of a Slanted-Tooth See-Through Labyrinth Seal to a Straight-Tooth See-Through Labyrinth Seal for Rotordynamic Coefficients and Leakage. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10825.

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

Council of Science Editors:

Mehta N. Comparison of a Slanted-Tooth See-Through Labyrinth Seal to a Straight-Tooth See-Through Labyrinth Seal for Rotordynamic Coefficients and Leakage. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10825

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


Texas A&M University

11. Jones, Nathan. The Importance of the Entropy Inequality on Numerical Simulations Using Reduced Methane-air Reaction Mechanisms.

Degree: 2012, Texas A&M University

 Many reaction mechanisms have been developed over the past few decades to predict flame characteristics. A detailed reaction mechanism can predict flame characteristics well, but… (more)

Subjects/Keywords: methane combustion; entropy inequality; reduced reaction mechanism

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APA (6th Edition):

Jones, N. (2012). The Importance of the Entropy Inequality on Numerical Simulations Using Reduced Methane-air Reaction Mechanisms. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11858

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):

Jones, Nathan. “The Importance of the Entropy Inequality on Numerical Simulations Using Reduced Methane-air Reaction Mechanisms.” 2012. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11858.

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

MLA Handbook (7th Edition):

Jones, Nathan. “The Importance of the Entropy Inequality on Numerical Simulations Using Reduced Methane-air Reaction Mechanisms.” 2012. Web. 18 Oct 2019.

Vancouver:

Jones N. The Importance of the Entropy Inequality on Numerical Simulations Using Reduced Methane-air Reaction Mechanisms. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11858.

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

Council of Science Editors:

Jones N. The Importance of the Entropy Inequality on Numerical Simulations Using Reduced Methane-air Reaction Mechanisms. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11858

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


Texas A&M University

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

Degree: 2008, Texas A&M University

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

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

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APA (6th Edition):

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

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):

Sahoo, Dipankar. “Experimental analysis of the vorticity and turbulent flow dynamics of a pitching airfoil at realistic flight (helicopter) conditions.” 2008. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/85893.

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

MLA Handbook (7th Edition):

Sahoo, Dipankar. “Experimental analysis of the vorticity and turbulent flow dynamics of a pitching airfoil at realistic flight (helicopter) conditions.” 2008. Web. 18 Oct 2019.

Vancouver:

Sahoo D. Experimental analysis of the vorticity and turbulent flow dynamics of a pitching airfoil at realistic flight (helicopter) conditions. [Internet] [Thesis]. Texas A&M University; 2008. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/85893.

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

Council of Science Editors:

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

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


Texas A&M University

13. Brown, Philip David. Measurement Versus Predictions of Rotordynamic Coefficients and Leakage Rates for a Hole-Pattern Gas Seal with Negative Preswirl.

Degree: 2012, Texas A&M University

 This thesis presents the results of high supply (up to 84 bar) pressure testing of hole-pattern annular gas seals performed at the Texas A &… (more)

Subjects/Keywords: negative preswirl; gas seal; hole-pattern seal; swirl brake

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APA (6th Edition):

Brown, P. D. (2012). Measurement Versus Predictions of Rotordynamic Coefficients and Leakage Rates for a Hole-Pattern Gas Seal with Negative Preswirl. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2011-08-9747

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):

Brown, Philip David. “Measurement Versus Predictions of Rotordynamic Coefficients and Leakage Rates for a Hole-Pattern Gas Seal with Negative Preswirl.” 2012. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2011-08-9747.

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

MLA Handbook (7th Edition):

Brown, Philip David. “Measurement Versus Predictions of Rotordynamic Coefficients and Leakage Rates for a Hole-Pattern Gas Seal with Negative Preswirl.” 2012. Web. 18 Oct 2019.

Vancouver:

Brown PD. Measurement Versus Predictions of Rotordynamic Coefficients and Leakage Rates for a Hole-Pattern Gas Seal with Negative Preswirl. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-08-9747.

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

Council of Science Editors:

Brown PD. Measurement Versus Predictions of Rotordynamic Coefficients and Leakage Rates for a Hole-Pattern Gas Seal with Negative Preswirl. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-08-9747

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


Texas A&M University

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

Degree: 2013, Texas A&M University

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

Subjects/Keywords: Small Wind Turbines

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APA (6th Edition):

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

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):

Soodavi, Moein. “Performance Study and Optimization of the Zephergy Wind Turbine.” 2013. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/151810.

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

MLA Handbook (7th Edition):

Soodavi, Moein. “Performance Study and Optimization of the Zephergy Wind Turbine.” 2013. Web. 18 Oct 2019.

Vancouver:

Soodavi M. Performance Study and Optimization of the Zephergy Wind Turbine. [Internet] [Thesis]. Texas A&M University; 2013. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/151810.

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

Council of Science Editors:

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

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


Texas A&M University

15. Gary, Keith William. Measurements of the Leakage and Rotordynamic Performance of Interlocking Labyrinth Seals.

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

 Annular-labyrinth seals restrict leakage in turbomachinery but may provide unwanted destabilizing forces. This work provides measurements of an interlockinglabyrinth gas seal to further the understanding… (more)

Subjects/Keywords: Rotordynamics; Turbomachinery; Labyrinth gas seals

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APA (6th Edition):

Gary, K. W. (2017). Measurements of the Leakage and Rotordynamic Performance of Interlocking Labyrinth Seals. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/169567

Chicago Manual of Style (16th Edition):

Gary, Keith William. “Measurements of the Leakage and Rotordynamic Performance of Interlocking Labyrinth Seals.” 2017. Masters Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/169567.

MLA Handbook (7th Edition):

Gary, Keith William. “Measurements of the Leakage and Rotordynamic Performance of Interlocking Labyrinth Seals.” 2017. Web. 18 Oct 2019.

Vancouver:

Gary KW. Measurements of the Leakage and Rotordynamic Performance of Interlocking Labyrinth Seals. [Internet] [Masters thesis]. Texas A&M University; 2017. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/169567.

Council of Science Editors:

Gary KW. Measurements of the Leakage and Rotordynamic Performance of Interlocking Labyrinth Seals. [Masters Thesis]. Texas A&M University; 2017. Available from: http://hdl.handle.net/1969.1/169567


Texas A&M University

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

Degree: 2016, Texas A&M University

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

Subjects/Keywords: Aeroservoelasticity; Unsteady Aerodynamics; Flutter Suppression

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APA (6th Edition):

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

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):

Suryakumar, Vishvas Samuel. “Fly-by-Feel Aeroservoelasticity.” 2016. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/159084.

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

MLA Handbook (7th Edition):

Suryakumar, Vishvas Samuel. “Fly-by-Feel Aeroservoelasticity.” 2016. Web. 18 Oct 2019.

Vancouver:

Suryakumar VS. Fly-by-Feel Aeroservoelasticity. [Internet] [Thesis]. Texas A&M University; 2016. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/159084.

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

Council of Science Editors:

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

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


Texas A&M University

17. Gargoloff, Joaquin Ivan. A numerical method for fully nonlinear aeroelastic analysis.

Degree: 2009, Texas A&M University

 This work presents a numerical method for the analysis of fully nonlinear aeroelastic problems. The aeroelastic model consisted of a Navier-Stokes flow solver, a nonlinear… (more)

Subjects/Keywords: aeroelasticity; cfd

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APA (6th Edition):

Gargoloff, J. I. (2009). A numerical method for fully nonlinear aeroelastic analysis. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1219

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):

Gargoloff, Joaquin Ivan. “A numerical method for fully nonlinear aeroelastic analysis.” 2009. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-1219.

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

MLA Handbook (7th Edition):

Gargoloff, Joaquin Ivan. “A numerical method for fully nonlinear aeroelastic analysis.” 2009. Web. 18 Oct 2019.

Vancouver:

Gargoloff JI. A numerical method for fully nonlinear aeroelastic analysis. [Internet] [Thesis]. Texas A&M University; 2009. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1219.

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

Council of Science Editors:

Gargoloff JI. A numerical method for fully nonlinear aeroelastic analysis. [Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1219

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


Texas A&M University

18. Freno, Brian Andrew. An Efficient Nonlinear Structural Dynamics Solver for Use in Computational Aeroelastic Analysis.

Degree: 2011, Texas A&M University

 Aerospace structures with large aspect ratio, such as airplane wings, rotorcraft blades, wind turbine blades, and jet engine fan and compressor blades, are particularly susceptible… (more)

Subjects/Keywords: aeroelasticity; nonlinear structural dynamics; computational aeroelasticity; elasticity; aerodynamics

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APA (6th Edition):

Freno, B. A. (2011). An Efficient Nonlinear Structural Dynamics Solver for Use in Computational Aeroelastic Analysis. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8039

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):

Freno, Brian Andrew. “An Efficient Nonlinear Structural Dynamics Solver for Use in Computational Aeroelastic Analysis.” 2011. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8039.

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

MLA Handbook (7th Edition):

Freno, Brian Andrew. “An Efficient Nonlinear Structural Dynamics Solver for Use in Computational Aeroelastic Analysis.” 2011. Web. 18 Oct 2019.

Vancouver:

Freno BA. An Efficient Nonlinear Structural Dynamics Solver for Use in Computational Aeroelastic Analysis. [Internet] [Thesis]. Texas A&M University; 2011. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8039.

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

Council of Science Editors:

Freno BA. An Efficient Nonlinear Structural Dynamics Solver for Use in Computational Aeroelastic Analysis. [Thesis]. Texas A&M University; 2011. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8039

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


Texas A&M University

19. Reyes, Dasia Ann. Advancing the Theoretical Foundation of the Partially-averaged Navier-Stokes Approach.

Degree: 2013, Texas A&M University

 The goal of this dissertation is to consolidate the theoretical foundation of variable-resolution (VR) methods in general and the partially-averaged Navier-Stokes (PANS) approach in particular.… (more)

Subjects/Keywords: PANS; Turbulence Modeling; Variable Resolution Methods; Bridging Methods

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APA (6th Edition):

Reyes, D. A. (2013). Advancing the Theoretical Foundation of the Partially-averaged Navier-Stokes Approach. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/149535

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):

Reyes, Dasia Ann. “Advancing the Theoretical Foundation of the Partially-averaged Navier-Stokes Approach.” 2013. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/149535.

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

MLA Handbook (7th Edition):

Reyes, Dasia Ann. “Advancing the Theoretical Foundation of the Partially-averaged Navier-Stokes Approach.” 2013. Web. 18 Oct 2019.

Vancouver:

Reyes DA. Advancing the Theoretical Foundation of the Partially-averaged Navier-Stokes Approach. [Internet] [Thesis]. Texas A&M University; 2013. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/149535.

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

Council of Science Editors:

Reyes DA. Advancing the Theoretical Foundation of the Partially-averaged Navier-Stokes Approach. [Thesis]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/149535

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


Texas A&M University

20. Ramakrishnan, Vijay. Development of an omni-directional weather-monitoring anemometer.

Degree: 2009, Texas A&M University

 This work presents the design, fabrication, calibration and testing of a pressure-based three-component anemometer capable of measuring accurate wind speeds in extreme weather conditions. The… (more)

Subjects/Keywords: anemometer; pressure probe; wind speed; 12-hole

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APA (6th Edition):

Ramakrishnan, V. (2009). Development of an omni-directional weather-monitoring anemometer. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/150920

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):

Ramakrishnan, Vijay. “Development of an omni-directional weather-monitoring anemometer.” 2009. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/150920.

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

MLA Handbook (7th Edition):

Ramakrishnan, Vijay. “Development of an omni-directional weather-monitoring anemometer.” 2009. Web. 18 Oct 2019.

Vancouver:

Ramakrishnan V. Development of an omni-directional weather-monitoring anemometer. [Internet] [Thesis]. Texas A&M University; 2009. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/150920.

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

Council of Science Editors:

Ramakrishnan V. Development of an omni-directional weather-monitoring anemometer. [Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/150920

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


Texas A&M University

21. Freno, Brian Andrew. Reduced-order Models for Computational Aeroelasticity.

Degree: 2013, Texas A&M University

 This dissertation presents a proper orthogonal decomposition (POD) method that uses dynamic basis functions. The dynamic functions are of a prescribed form and do not… (more)

Subjects/Keywords: Proper orthogonal decomposition; Reduced-order modeling; Deforming mesh; Dynamic basis functions; Computational fluid dynamics; Grassmann manifold

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APA (6th Edition):

Freno, B. A. (2013). Reduced-order Models for Computational Aeroelasticity. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/151757

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):

Freno, Brian Andrew. “Reduced-order Models for Computational Aeroelasticity.” 2013. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/151757.

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

MLA Handbook (7th Edition):

Freno, Brian Andrew. “Reduced-order Models for Computational Aeroelasticity.” 2013. Web. 18 Oct 2019.

Vancouver:

Freno BA. Reduced-order Models for Computational Aeroelasticity. [Internet] [Thesis]. Texas A&M University; 2013. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/151757.

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

Council of Science Editors:

Freno BA. Reduced-order Models for Computational Aeroelasticity. [Thesis]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/151757

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


Texas A&M University

22. Cooper, Jacob. Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics.

Degree: 2014, Texas A&M University

 This dissertation investigates high angle of attack delta wing flow at multiple resolutions of turbulence closure. The work is divided into four studies. The objectives… (more)

Subjects/Keywords: delta wing; diamond wing; turbulence model; PANS

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APA (6th Edition):

Cooper, J. (2014). Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/153426

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):

Cooper, Jacob. “Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics.” 2014. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/153426.

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

MLA Handbook (7th Edition):

Cooper, Jacob. “Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics.” 2014. Web. 18 Oct 2019.

Vancouver:

Cooper J. Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics. [Internet] [Thesis]. Texas A&M University; 2014. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/153426.

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

Council of Science Editors:

Cooper J. Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics. [Thesis]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/153426

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


Texas A&M University

23. Scholten, William David. Analysis and Wind Tunnel Testing of a Superelastic Slat-Cove Filler for Airframe Noise Reduction.

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

 During low speed maneuvers, such as landing and approach, a significant portion of the noise generated by transport aircraft is due to airframe noise. The… (more)

Subjects/Keywords: SMA; FSI; CFD; Wind Tunnel

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APA (6th Edition):

Scholten, W. D. (2016). Analysis and Wind Tunnel Testing of a Superelastic Slat-Cove Filler for Airframe Noise Reduction. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/159068

Chicago Manual of Style (16th Edition):

Scholten, William David. “Analysis and Wind Tunnel Testing of a Superelastic Slat-Cove Filler for Airframe Noise Reduction.” 2016. Masters Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/159068.

MLA Handbook (7th Edition):

Scholten, William David. “Analysis and Wind Tunnel Testing of a Superelastic Slat-Cove Filler for Airframe Noise Reduction.” 2016. Web. 18 Oct 2019.

Vancouver:

Scholten WD. Analysis and Wind Tunnel Testing of a Superelastic Slat-Cove Filler for Airframe Noise Reduction. [Internet] [Masters thesis]. Texas A&M University; 2016. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/159068.

Council of Science Editors:

Scholten WD. Analysis and Wind Tunnel Testing of a Superelastic Slat-Cove Filler for Airframe Noise Reduction. [Masters Thesis]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/159068


Texas A&M University

24. Ream, Allen. Creating Reduced Order Methane-Air Combustion Mechanisms That Satisfy the Differential Entropy Inequality.

Degree: 2015, Texas A&M University

 To simulate the combustion of a flame, or any reacting fluid flow, it is necessary to incorporate a reaction mechanism which describes the incremental steps… (more)

Subjects/Keywords: combustion; reduced mechanism; differential entropy inequality

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APA (6th Edition):

Ream, A. (2015). Creating Reduced Order Methane-Air Combustion Mechanisms That Satisfy the Differential Entropy Inequality. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/156362

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):

Ream, Allen. “Creating Reduced Order Methane-Air Combustion Mechanisms That Satisfy the Differential Entropy Inequality.” 2015. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/156362.

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

MLA Handbook (7th Edition):

Ream, Allen. “Creating Reduced Order Methane-Air Combustion Mechanisms That Satisfy the Differential Entropy Inequality.” 2015. Web. 18 Oct 2019.

Vancouver:

Ream A. Creating Reduced Order Methane-Air Combustion Mechanisms That Satisfy the Differential Entropy Inequality. [Internet] [Thesis]. Texas A&M University; 2015. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/156362.

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

Council of Science Editors:

Ream A. Creating Reduced Order Methane-Air Combustion Mechanisms That Satisfy the Differential Entropy Inequality. [Thesis]. Texas A&M University; 2015. Available from: http://hdl.handle.net/1969.1/156362

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


Texas A&M University

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

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

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

Subjects/Keywords: Computational Fluid Dynamcs; Turbomachinery

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Carpenter IV, Forrest Lafon. “Practical Aspects of Computational Fluid Dynamics for Turbomachinery.” 2016. Doctoral Dissertation, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/158055.

MLA Handbook (7th Edition):

Carpenter IV, Forrest Lafon. “Practical Aspects of Computational Fluid Dynamics for Turbomachinery.” 2016. Web. 18 Oct 2019.

Vancouver:

Carpenter IV FL. Practical Aspects of Computational Fluid Dynamics for Turbomachinery. [Internet] [Doctoral dissertation]. Texas A&M University; 2016. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/158055.

Council of Science Editors:

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


Texas A&M University

26. Brown II, Robert Lee. Numerical Simulations of Hypersonic Aerothermoelastic Phenomena.

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

 This dissertation examines the following subjects important to hypersonic aerothermoelastic flows: aerodynamic heating on a double-wedge airfoil, active cooling on a double-wedge airfoil, and aerothermoelastic… (more)

Subjects/Keywords: hypersonic; panel flutter; aerothermal; aeroelastic; aerothermoelastic; simulation

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APA (6th Edition):

Brown II, R. L. (2016). Numerical Simulations of Hypersonic Aerothermoelastic Phenomena. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/158046

Chicago Manual of Style (16th Edition):

Brown II, Robert Lee. “Numerical Simulations of Hypersonic Aerothermoelastic Phenomena.” 2016. Doctoral Dissertation, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/158046.

MLA Handbook (7th Edition):

Brown II, Robert Lee. “Numerical Simulations of Hypersonic Aerothermoelastic Phenomena.” 2016. Web. 18 Oct 2019.

Vancouver:

Brown II RL. Numerical Simulations of Hypersonic Aerothermoelastic Phenomena. [Internet] [Doctoral dissertation]. Texas A&M University; 2016. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/158046.

Council of Science Editors:

Brown II RL. Numerical Simulations of Hypersonic Aerothermoelastic Phenomena. [Doctoral Dissertation]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/158046


Texas A&M University

27. Liliedahl, David Noel. A Time-linearized Navier-Stokes Solver for Annular Gas Seal Rotordynamic Analysis.

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

 A time-linearized CFD solver for analyzing rotordynamics of gas seals is presented offering an improvement over existing linearized CFD solvers. Previous linearized solvers required structured… (more)

Subjects/Keywords: CFD; Time-Linearized; Linearized; Navier-Stokes; Rotordynamics

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

APA (6th Edition):

Liliedahl, D. N. (2017). A Time-linearized Navier-Stokes Solver for Annular Gas Seal Rotordynamic Analysis. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/165793

Chicago Manual of Style (16th Edition):

Liliedahl, David Noel. “A Time-linearized Navier-Stokes Solver for Annular Gas Seal Rotordynamic Analysis.” 2017. Doctoral Dissertation, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/165793.

MLA Handbook (7th Edition):

Liliedahl, David Noel. “A Time-linearized Navier-Stokes Solver for Annular Gas Seal Rotordynamic Analysis.” 2017. Web. 18 Oct 2019.

Vancouver:

Liliedahl DN. A Time-linearized Navier-Stokes Solver for Annular Gas Seal Rotordynamic Analysis. [Internet] [Doctoral dissertation]. Texas A&M University; 2017. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/165793.

Council of Science Editors:

Liliedahl DN. A Time-linearized Navier-Stokes Solver for Annular Gas Seal Rotordynamic Analysis. [Doctoral Dissertation]. Texas A&M University; 2017. Available from: http://hdl.handle.net/1969.1/165793

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

Degree: 2009, Texas A&M University

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

Subjects/Keywords: flow control; aerodynamics; inlet duct

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

APA (6th Edition):

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

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):

Kumar, Abhinav. “Flow control optimization in a jet engine serpentine inlet duct.” 2009. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-1399.

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

MLA Handbook (7th Edition):

Kumar, Abhinav. “Flow control optimization in a jet engine serpentine inlet duct.” 2009. Web. 18 Oct 2019.

Vancouver:

Kumar A. Flow control optimization in a jet engine serpentine inlet duct. [Internet] [Thesis]. Texas A&M University; 2009. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1399.

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

Council of Science Editors:

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

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

29. Fontenot, Raymond Lee. Advances in Reduced-Order Modeling Based on Proper Orthogonal Decomposition for Single and Two-Phase Flows.

Degree: 2012, Texas A&M University

 This thesis presents advances in reduced-order modeling based on proper orthogonal decomposition (POD) for single and two-phase flows. Reduced-order models (ROMs) are generated for two-phase… (more)

Subjects/Keywords: Proper Orthogonal Decomposition; Reduced-Order Models; Mathematical Morphology

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

APA (6th Edition):

Fontenot, R. L. (2012). Advances in Reduced-Order Modeling Based on Proper Orthogonal Decomposition for Single and Two-Phase Flows. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-12-8750

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):

Fontenot, Raymond Lee. “Advances in Reduced-Order Modeling Based on Proper Orthogonal Decomposition for Single and Two-Phase Flows.” 2012. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2010-12-8750.

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

MLA Handbook (7th Edition):

Fontenot, Raymond Lee. “Advances in Reduced-Order Modeling Based on Proper Orthogonal Decomposition for Single and Two-Phase Flows.” 2012. Web. 18 Oct 2019.

Vancouver:

Fontenot RL. Advances in Reduced-Order Modeling Based on Proper Orthogonal Decomposition for Single and Two-Phase Flows. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-12-8750.

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

Council of Science Editors:

Fontenot RL. Advances in Reduced-Order Modeling Based on Proper Orthogonal Decomposition for Single and Two-Phase Flows. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-12-8750

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

30. Wilkes, Jason Christopher. Measured and Predicted Rotor-Pad Transfer Functions for a Rocker-Pivot Tilting-Pad Journal Bearing.

Degree: 2012, Texas A&M University

 Many researchers have compared predicted stiffness and damping coefficients for tilting-pad journal bearings (TPJBs) to measurements. Most have found that direct damping is consistently overpredicted.… (more)

Subjects/Keywords: pad; tilting pad journal bearing; pad motion; transfer functions; rotordynamics; experimental; bearing test; bearing impedance

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

APA (6th Edition):

Wilkes, J. C. (2012). Measured and Predicted Rotor-Pad Transfer Functions for a Rocker-Pivot Tilting-Pad Journal Bearing. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10366

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):

Wilkes, Jason Christopher. “Measured and Predicted Rotor-Pad Transfer Functions for a Rocker-Pivot Tilting-Pad Journal Bearing.” 2012. Thesis, Texas A&M University. Accessed October 18, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10366.

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

MLA Handbook (7th Edition):

Wilkes, Jason Christopher. “Measured and Predicted Rotor-Pad Transfer Functions for a Rocker-Pivot Tilting-Pad Journal Bearing.” 2012. Web. 18 Oct 2019.

Vancouver:

Wilkes JC. Measured and Predicted Rotor-Pad Transfer Functions for a Rocker-Pivot Tilting-Pad Journal Bearing. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10366.

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

Council of Science Editors:

Wilkes JC. Measured and Predicted Rotor-Pad Transfer Functions for a Rocker-Pivot Tilting-Pad Journal Bearing. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10366

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

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