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You searched for subject:(Aerospace Engineering). Showing records 1 – 30 of 4365 total matches.

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Texas A&M University

1. Kim, Hye-Young. Symbolic methods for general-purpose and class specific formulation of multibody equations of motion.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 The difficulty of design and control of complicated multibody dynamical systems in mechanical and aerospace engineering requires numerical simulations and has led to development of… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Kim, H. (2012). Symbolic methods for general-purpose and class specific formulation of multibody equations of motion. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-K563

Chicago Manual of Style (16th Edition):

Kim, Hye-Young. “Symbolic methods for general-purpose and class specific formulation of multibody equations of motion.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-K563.

MLA Handbook (7th Edition):

Kim, Hye-Young. “Symbolic methods for general-purpose and class specific formulation of multibody equations of motion.” 2012. Web. 20 Sep 2017.

Vancouver:

Kim H. Symbolic methods for general-purpose and class specific formulation of multibody equations of motion. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-K563.

Council of Science Editors:

Kim H. Symbolic methods for general-purpose and class specific formulation of multibody equations of motion. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-K563


Texas A&M University

2. Kinser Robert Eric. Development of neural network calibration algorithms for multi-port pressure probes.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 The development of an enhanced neural network training algorithm and program for the calibration of velocity measurement instrumentation is presented. The backpropagation-based program, PROBENET, is… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Eric, K. R. (2012). Development of neural network calibration algorithms for multi-port pressure probes. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-K57

Chicago Manual of Style (16th Edition):

Eric, Kinser Robert. “Development of neural network calibration algorithms for multi-port pressure probes.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-K57.

MLA Handbook (7th Edition):

Eric, Kinser Robert. “Development of neural network calibration algorithms for multi-port pressure probes.” 2012. Web. 20 Sep 2017.

Vancouver:

Eric KR. Development of neural network calibration algorithms for multi-port pressure probes. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-K57.

Council of Science Editors:

Eric KR. Development of neural network calibration algorithms for multi-port pressure probes. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-K57


Texas A&M University

3. McCann, Barrett Taylor. Evaluation of local preconditioners for multigrid solutions of the compressible Euler equations.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 The goal of this study is to examine and compare the effectiveness of two local preconditioners, when used in a multigrid algorithm, in accelerating the… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

McCann, B. T. (2012). Evaluation of local preconditioners for multigrid solutions of the compressible Euler equations. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-M326

Chicago Manual of Style (16th Edition):

McCann, Barrett Taylor. “Evaluation of local preconditioners for multigrid solutions of the compressible Euler equations.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-M326.

MLA Handbook (7th Edition):

McCann, Barrett Taylor. “Evaluation of local preconditioners for multigrid solutions of the compressible Euler equations.” 2012. Web. 20 Sep 2017.

Vancouver:

McCann BT. Evaluation of local preconditioners for multigrid solutions of the compressible Euler equations. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-M326.

Council of Science Editors:

McCann BT. Evaluation of local preconditioners for multigrid solutions of the compressible Euler equations. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-M326


Texas A&M University

4. Mani, Somnath. A reduced Blade-Vortex Interaction rotor.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 This research work aims at mapping the BVI azimuthal locations using a model rotor. A model rotor was first developed. An experimental investigation was then… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Mani, S. (2012). A reduced Blade-Vortex Interaction rotor. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-M362

Chicago Manual of Style (16th Edition):

Mani, Somnath. “A reduced Blade-Vortex Interaction rotor.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-M362.

MLA Handbook (7th Edition):

Mani, Somnath. “A reduced Blade-Vortex Interaction rotor.” 2012. Web. 20 Sep 2017.

Vancouver:

Mani S. A reduced Blade-Vortex Interaction rotor. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-M362.

Council of Science Editors:

Mani S. A reduced Blade-Vortex Interaction rotor. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-M362


Texas A&M University

5. Nguyen, Thinh Xuan. A neural network mode inference engine for the advisory system for training and safety.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 To improve the safety record of the private general aviation sector, the Advisory System for Training and Safety (ASTRAS) was conceived. The ASTRAS software provides… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Nguyen, T. X. (2012). A neural network mode inference engine for the advisory system for training and safety. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-N47

Chicago Manual of Style (16th Edition):

Nguyen, Thinh Xuan. “A neural network mode inference engine for the advisory system for training and safety.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-N47.

MLA Handbook (7th Edition):

Nguyen, Thinh Xuan. “A neural network mode inference engine for the advisory system for training and safety.” 2012. Web. 20 Sep 2017.

Vancouver:

Nguyen TX. A neural network mode inference engine for the advisory system for training and safety. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-N47.

Council of Science Editors:

Nguyen TX. A neural network mode inference engine for the advisory system for training and safety. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-N47


Texas A&M University

6. Pisor, Robert Donald. Design and analysis of large deformation spiral springs.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 This thesis presents the analysis, design and construction of spiral springs for use in the Microgravity Simulator at Phillips Laboratory at Kirkland AFB in New… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Pisor, R. D. (2012). Design and analysis of large deformation spiral springs. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-P57

Chicago Manual of Style (16th Edition):

Pisor, Robert Donald. “Design and analysis of large deformation spiral springs.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-P57.

MLA Handbook (7th Edition):

Pisor, Robert Donald. “Design and analysis of large deformation spiral springs.” 2012. Web. 20 Sep 2017.

Vancouver:

Pisor RD. Design and analysis of large deformation spiral springs. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-P57.

Council of Science Editors:

Pisor RD. Design and analysis of large deformation spiral springs. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-P57


Texas A&M University

7. Sundstrom, Keith Andrew. Stress analysis of a hybrid composite drilling riser.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 Methods to thoroughly and efficiently analyze a composite riser designed for use in offshore drilling applications and subjected to various types of loading have been… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Sundstrom, K. A. (2012). Stress analysis of a hybrid composite drilling riser. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-S87

Chicago Manual of Style (16th Edition):

Sundstrom, Keith Andrew. “Stress analysis of a hybrid composite drilling riser.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-S87.

MLA Handbook (7th Edition):

Sundstrom, Keith Andrew. “Stress analysis of a hybrid composite drilling riser.” 2012. Web. 20 Sep 2017.

Vancouver:

Sundstrom KA. Stress analysis of a hybrid composite drilling riser. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-S87.

Council of Science Editors:

Sundstrom KA. Stress analysis of a hybrid composite drilling riser. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-S87


Texas A&M University

8. Datta, Dibyendu Kumar, Dd 1973-. A-posteriori estimation and adaptive control of the error in the solution quantity of interest.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 The engineers are primarily interested in quantities like stresses and displacements in the critical regions, the stress intensity factor at the crack-tip of an initiated… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Datta, Dibyendu Kumar, D. 1. (2012). A-posteriori estimation and adaptive control of the error in the solution quantity of interest. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1997-THESIS-D37

Chicago Manual of Style (16th Edition):

Datta, Dibyendu Kumar, Dd 1973-. “A-posteriori estimation and adaptive control of the error in the solution quantity of interest.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-1997-THESIS-D37.

MLA Handbook (7th Edition):

Datta, Dibyendu Kumar, Dd 1973-. “A-posteriori estimation and adaptive control of the error in the solution quantity of interest.” 2012. Web. 20 Sep 2017.

Vancouver:

Datta, Dibyendu Kumar D1. A-posteriori estimation and adaptive control of the error in the solution quantity of interest. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1997-THESIS-D37.

Council of Science Editors:

Datta, Dibyendu Kumar D1. A-posteriori estimation and adaptive control of the error in the solution quantity of interest. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1997-THESIS-D37


Texas A&M University

9. Foulk, James Wesley. A model for predicting the damage and oxidation dependent life of SCS-6/Ti-B21S [0]4 metal matrix composite.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 A method for predicting the life of an embrittled metal matrix composite using the finite element method coupled with models for material inelasticity, surface embrittlement,… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Foulk, J. W. (2012). A model for predicting the damage and oxidation dependent life of SCS-6/Ti-B21S [0]4 metal matrix composite. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1997-THESIS-F68

Chicago Manual of Style (16th Edition):

Foulk, James Wesley. “A model for predicting the damage and oxidation dependent life of SCS-6/Ti-B21S [0]4 metal matrix composite.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-1997-THESIS-F68.

MLA Handbook (7th Edition):

Foulk, James Wesley. “A model for predicting the damage and oxidation dependent life of SCS-6/Ti-B21S [0]4 metal matrix composite.” 2012. Web. 20 Sep 2017.

Vancouver:

Foulk JW. A model for predicting the damage and oxidation dependent life of SCS-6/Ti-B21S [0]4 metal matrix composite. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1997-THESIS-F68.

Council of Science Editors:

Foulk JW. A model for predicting the damage and oxidation dependent life of SCS-6/Ti-B21S [0]4 metal matrix composite. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1997-THESIS-F68


Texas A&M University

10. Gilliatt, Heather Colleen. Investigations of internal resonance phenomena and related nonlinear pathologies in aeroelastic systems.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 The main goal of this research is to investigate the presence of internal resonance in aeroelastic structures, and to illustrate the effects internal resonance may… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Gilliatt, H. C. (2012). Investigations of internal resonance phenomena and related nonlinear pathologies in aeroelastic systems. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1997-THESIS-G534

Chicago Manual of Style (16th Edition):

Gilliatt, Heather Colleen. “Investigations of internal resonance phenomena and related nonlinear pathologies in aeroelastic systems.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-1997-THESIS-G534.

MLA Handbook (7th Edition):

Gilliatt, Heather Colleen. “Investigations of internal resonance phenomena and related nonlinear pathologies in aeroelastic systems.” 2012. Web. 20 Sep 2017.

Vancouver:

Gilliatt HC. Investigations of internal resonance phenomena and related nonlinear pathologies in aeroelastic systems. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1997-THESIS-G534.

Council of Science Editors:

Gilliatt HC. Investigations of internal resonance phenomena and related nonlinear pathologies in aeroelastic systems. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1997-THESIS-G534


Texas A&M University

11. Gilarranz, Jose Luis. Development of a high-frame-rate high-resolution particle image velocimetry system and applications to the characterization of synthetic jet actuators.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 This thesis presents the hardware development for two high-frame-rate particle image velocimetry systems. One of them is based on the use of a high-speed film… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Gilarranz, J. L. (2012). Development of a high-frame-rate high-resolution particle image velocimetry system and applications to the characterization of synthetic jet actuators. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-G55

Chicago Manual of Style (16th Edition):

Gilarranz, Jose Luis. “Development of a high-frame-rate high-resolution particle image velocimetry system and applications to the characterization of synthetic jet actuators.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-G55.

MLA Handbook (7th Edition):

Gilarranz, Jose Luis. “Development of a high-frame-rate high-resolution particle image velocimetry system and applications to the characterization of synthetic jet actuators.” 2012. Web. 20 Sep 2017.

Vancouver:

Gilarranz JL. Development of a high-frame-rate high-resolution particle image velocimetry system and applications to the characterization of synthetic jet actuators. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-G55.

Council of Science Editors:

Gilarranz JL. Development of a high-frame-rate high-resolution particle image velocimetry system and applications to the characterization of synthetic jet actuators. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-G55


Texas A&M University

12. Honea, Mark Stephen. An analysis of electrothermodynamic heating and cooling.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 Current advances in semiconductor manufacturing have brought about an increasing use of thermoelectricity in a variety of applications. Most of these applications, however, have involved… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Honea, M. S. (2012). An analysis of electrothermodynamic heating and cooling. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-H66

Chicago Manual of Style (16th Edition):

Honea, Mark Stephen. “An analysis of electrothermodynamic heating and cooling.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-H66.

MLA Handbook (7th Edition):

Honea, Mark Stephen. “An analysis of electrothermodynamic heating and cooling.” 2012. Web. 20 Sep 2017.

Vancouver:

Honea MS. An analysis of electrothermodynamic heating and cooling. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-H66.

Council of Science Editors:

Honea MS. An analysis of electrothermodynamic heating and cooling. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-H66


Texas A&M University

13. Huang, Haiming. Identification and control of a flexible structure.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 This thesis describes the identification and vibration ics. control of a cantilevered beam with piezoelectric material as actuators and sensors. The Euler-Bernoulli beam equation is… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Huang, H. (2012). Identification and control of a flexible structure. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-H825

Chicago Manual of Style (16th Edition):

Huang, Haiming. “Identification and control of a flexible structure.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-H825.

MLA Handbook (7th Edition):

Huang, Haiming. “Identification and control of a flexible structure.” 2012. Web. 20 Sep 2017.

Vancouver:

Huang H. Identification and control of a flexible structure. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-H825.

Council of Science Editors:

Huang H. Identification and control of a flexible structure. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-H825


Texas A&M University

14. Johansen, Espen S. Steady and unsteady calibration of multi-hole probes.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 This thesis presents the development of a data crographics. reduction algorithm for multi-hole pressure probes. The algorithm has been developed for the reduction of calibration… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Johansen, E. S. (2012). Steady and unsteady calibration of multi-hole probes. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-J63

Chicago Manual of Style (16th Edition):

Johansen, Espen S. “Steady and unsteady calibration of multi-hole probes.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-J63.

MLA Handbook (7th Edition):

Johansen, Espen S. “Steady and unsteady calibration of multi-hole probes.” 2012. Web. 20 Sep 2017.

Vancouver:

Johansen ES. Steady and unsteady calibration of multi-hole probes. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-J63.

Council of Science Editors:

Johansen ES. Steady and unsteady calibration of multi-hole probes. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-J63


Texas A&M University

15. Jung, Hee. Development of a rules-based advisory system for detecting off-nominal behavior of spacecraft digital autopilots.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 based advisory system for detecting off-nominal behavior of spacecraft digital autopilots(DAP) in real-time. The DAP of the space shuttle is used as a simulation model… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Jung, H. (2012). Development of a rules-based advisory system for detecting off-nominal behavior of spacecraft digital autopilots. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-J863

Chicago Manual of Style (16th Edition):

Jung, Hee. “Development of a rules-based advisory system for detecting off-nominal behavior of spacecraft digital autopilots.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-J863.

MLA Handbook (7th Edition):

Jung, Hee. “Development of a rules-based advisory system for detecting off-nominal behavior of spacecraft digital autopilots.” 2012. Web. 20 Sep 2017.

Vancouver:

Jung H. Development of a rules-based advisory system for detecting off-nominal behavior of spacecraft digital autopilots. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-J863.

Council of Science Editors:

Jung H. Development of a rules-based advisory system for detecting off-nominal behavior of spacecraft digital autopilots. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-J863


Texas A&M University

16. Collard, Joseph Eugene. Blade-forced vibration effects in turbomachinery rotor-stator interaction.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 This thesis presents the effects of blade-forced vibration in turbomachinery rotor-stator interaction. A quasi-three-dimensional multi-row analysis, based on an Euler/Navier-Stokes solver and a parallel computational… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Collard, J. E. (2012). Blade-forced vibration effects in turbomachinery rotor-stator interaction. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-C625

Chicago Manual of Style (16th Edition):

Collard, Joseph Eugene. “Blade-forced vibration effects in turbomachinery rotor-stator interaction.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-C625.

MLA Handbook (7th Edition):

Collard, Joseph Eugene. “Blade-forced vibration effects in turbomachinery rotor-stator interaction.” 2012. Web. 20 Sep 2017.

Vancouver:

Collard JE. Blade-forced vibration effects in turbomachinery rotor-stator interaction. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-C625.

Council of Science Editors:

Collard JE. Blade-forced vibration effects in turbomachinery rotor-stator interaction. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-C625


Texas A&M University

17. Damiana, Thomas Anthony. An experimental investigation of the mean flow field of a wavy cylinder at critical Reynolds numbers.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 Fluid flow around a wavy cylinder geometry was investigated in the Texas A&M University 2'x3' wind tunnel. Tests consisted of mean surface static pressure and… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Damiana, T. A. (2012). An experimental investigation of the mean flow field of a wavy cylinder at critical Reynolds numbers. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1994-THESIS-D158

Chicago Manual of Style (16th Edition):

Damiana, Thomas Anthony. “An experimental investigation of the mean flow field of a wavy cylinder at critical Reynolds numbers.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-1994-THESIS-D158.

MLA Handbook (7th Edition):

Damiana, Thomas Anthony. “An experimental investigation of the mean flow field of a wavy cylinder at critical Reynolds numbers.” 2012. Web. 20 Sep 2017.

Vancouver:

Damiana TA. An experimental investigation of the mean flow field of a wavy cylinder at critical Reynolds numbers. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1994-THESIS-D158.

Council of Science Editors:

Damiana TA. An experimental investigation of the mean flow field of a wavy cylinder at critical Reynolds numbers. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1994-THESIS-D158


Texas A&M University

18. Day, Nathan Allan. Ultrasonic wave propagation through a layer of spherical inclusions with random of periodic arrangements.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 This thesis presents experimental results obtained by examining ultrasonic wave propagation through a layer of spherical lead inclusions embedded in a polyester matrix. Through transmission… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Day, N. A. (2012). Ultrasonic wave propagation through a layer of spherical inclusions with random of periodic arrangements. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1994-THESIS-D273

Chicago Manual of Style (16th Edition):

Day, Nathan Allan. “Ultrasonic wave propagation through a layer of spherical inclusions with random of periodic arrangements.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-1994-THESIS-D273.

MLA Handbook (7th Edition):

Day, Nathan Allan. “Ultrasonic wave propagation through a layer of spherical inclusions with random of periodic arrangements.” 2012. Web. 20 Sep 2017.

Vancouver:

Day NA. Ultrasonic wave propagation through a layer of spherical inclusions with random of periodic arrangements. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1994-THESIS-D273.

Council of Science Editors:

Day NA. Ultrasonic wave propagation through a layer of spherical inclusions with random of periodic arrangements. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1994-THESIS-D273


Texas A&M University

19. Oryu, Hiroshi. Study of active control of instability in a boundary layer over a flat plate flow.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 A feasibility study of utilizing synthetic jet actuators as a mean to mitigate disturbances that can cause instability and turbulent flow is described. Prediction of… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Oryu, H. (2012). Study of active control of instability in a boundary layer over a flat plate flow. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-O79

Chicago Manual of Style (16th Edition):

Oryu, Hiroshi. “Study of active control of instability in a boundary layer over a flat plate flow.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-O79.

MLA Handbook (7th Edition):

Oryu, Hiroshi. “Study of active control of instability in a boundary layer over a flat plate flow.” 2012. Web. 20 Sep 2017.

Vancouver:

Oryu H. Study of active control of instability in a boundary layer over a flat plate flow. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-O79.

Council of Science Editors:

Oryu H. Study of active control of instability in a boundary layer over a flat plate flow. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-O79


Texas A&M University

20. Rao, Preetham P. Active flow separation control using synthetic jet actuators.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 The use of synthetic jet actuators for controlling the boundary layer flow and flow separation over a wing is investigated. A theory for the optimum… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Rao, P. P. (2012). Active flow separation control using synthetic jet actuators. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-R37

Chicago Manual of Style (16th Edition):

Rao, Preetham P. “Active flow separation control using synthetic jet actuators.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-R37.

MLA Handbook (7th Edition):

Rao, Preetham P. “Active flow separation control using synthetic jet actuators.” 2012. Web. 20 Sep 2017.

Vancouver:

Rao PP. Active flow separation control using synthetic jet actuators. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-R37.

Council of Science Editors:

Rao PP. Active flow separation control using synthetic jet actuators. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-R37


Texas A&M University

21. Samaan, Malak Anees. Studies in robust control systems with application to various spacecraft attitude control schemes.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 A robust control system remains stable under perturbations. In the last two decades, robust control has become one of the most important fields in testing… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Samaan, M. A. (2012). Studies in robust control systems with application to various spacecraft attitude control schemes. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-S24

Chicago Manual of Style (16th Edition):

Samaan, Malak Anees. “Studies in robust control systems with application to various spacecraft attitude control schemes.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-S24.

MLA Handbook (7th Edition):

Samaan, Malak Anees. “Studies in robust control systems with application to various spacecraft attitude control schemes.” 2012. Web. 20 Sep 2017.

Vancouver:

Samaan MA. Studies in robust control systems with application to various spacecraft attitude control schemes. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-S24.

Council of Science Editors:

Samaan MA. Studies in robust control systems with application to various spacecraft attitude control schemes. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-S24


Texas A&M University

22. Smith, David Matthew. Agility metric sensitivity using linear error theory.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 Aircraft agility metrics have been proposed for use to measure the performance and capability of aircraft onboard while in-flight. The sensitivity of these metrics to… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Smith, D. M. (2012). Agility metric sensitivity using linear error theory. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-S613

Chicago Manual of Style (16th Edition):

Smith, David Matthew. “Agility metric sensitivity using linear error theory.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-S613.

MLA Handbook (7th Edition):

Smith, David Matthew. “Agility metric sensitivity using linear error theory.” 2012. Web. 20 Sep 2017.

Vancouver:

Smith DM. Agility metric sensitivity using linear error theory. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-S613.

Council of Science Editors:

Smith DM. Agility metric sensitivity using linear error theory. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-S613


Texas A&M University

23. Wilkins, Matthew Paul. Characterizing orbit uncertainty due to atmospheric uncertainty.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 In orbit prediction, there exists a need for accurate estimates of the accuracy of a prediction, i.e. the covariance. An accurate covariance is required for… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Wilkins, M. P. (2012). Characterizing orbit uncertainty due to atmospheric uncertainty. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-W343

Chicago Manual of Style (16th Edition):

Wilkins, Matthew Paul. “Characterizing orbit uncertainty due to atmospheric uncertainty.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-W343.

MLA Handbook (7th Edition):

Wilkins, Matthew Paul. “Characterizing orbit uncertainty due to atmospheric uncertainty.” 2012. Web. 20 Sep 2017.

Vancouver:

Wilkins MP. Characterizing orbit uncertainty due to atmospheric uncertainty. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-W343.

Council of Science Editors:

Wilkins MP. Characterizing orbit uncertainty due to atmospheric uncertainty. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-W343


Texas A&M University

24. Wilson, Larry Nixon. Development of a shape memory alloy actuated biomimetic hydrofoil.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 The development of an active biomimetic hydrofoil that utilizes Shape Memory Alloy (SMA) actuator technology is presented herein. This work describes the design and testing… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Wilson, L. N. (2012). Development of a shape memory alloy actuated biomimetic hydrofoil. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-W36

Chicago Manual of Style (16th Edition):

Wilson, Larry Nixon. “Development of a shape memory alloy actuated biomimetic hydrofoil.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-W36.

MLA Handbook (7th Edition):

Wilson, Larry Nixon. “Development of a shape memory alloy actuated biomimetic hydrofoil.” 2012. Web. 20 Sep 2017.

Vancouver:

Wilson LN. Development of a shape memory alloy actuated biomimetic hydrofoil. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-W36.

Council of Science Editors:

Wilson LN. Development of a shape memory alloy actuated biomimetic hydrofoil. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-W36


Texas A&M University

25. Alonso, Roberto Jorge. Relative navigation for formation flying of spacecraft.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 The objective of this thesis is to develop an efficient and robust approach for relative navigation and attitude estimation of spacecraft flying in formation. The… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Alonso, R. J. (2012). Relative navigation for formation flying of spacecraft. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-A453

Chicago Manual of Style (16th Edition):

Alonso, Roberto Jorge. “Relative navigation for formation flying of spacecraft.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-A453.

MLA Handbook (7th Edition):

Alonso, Roberto Jorge. “Relative navigation for formation flying of spacecraft.” 2012. Web. 20 Sep 2017.

Vancouver:

Alonso RJ. Relative navigation for formation flying of spacecraft. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-A453.

Council of Science Editors:

Alonso RJ. Relative navigation for formation flying of spacecraft. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-A453


Texas A&M University

26. Bryson, Amy Louise. Optimal command generation for maneuvering the space station.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 The objective of this research is to obtain near minimum-fuel and minimum-time maneuver commands for large-angle maneuvers for the international space station. Attitude and angular… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Bryson, A. L. (2012). Optimal command generation for maneuvering the space station. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-B79

Chicago Manual of Style (16th Edition):

Bryson, Amy Louise. “Optimal command generation for maneuvering the space station.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-B79.

MLA Handbook (7th Edition):

Bryson, Amy Louise. “Optimal command generation for maneuvering the space station.” 2012. Web. 20 Sep 2017.

Vancouver:

Bryson AL. Optimal command generation for maneuvering the space station. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-B79.

Council of Science Editors:

Bryson AL. Optimal command generation for maneuvering the space station. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-B79


Texas A&M University

27. Clayton, Kyle Martin. Mechanical modeling of the plastic bonded explosive LX17.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 The current research attempts to develop a model for a polycrystalline, composite solid with viscoelastic matrix known as LX17. It is a highly-filled plastic bonded… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Clayton, K. M. (2012). Mechanical modeling of the plastic bonded explosive LX17. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-C532

Chicago Manual of Style (16th Edition):

Clayton, Kyle Martin. “Mechanical modeling of the plastic bonded explosive LX17.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-C532.

MLA Handbook (7th Edition):

Clayton, Kyle Martin. “Mechanical modeling of the plastic bonded explosive LX17.” 2012. Web. 20 Sep 2017.

Vancouver:

Clayton KM. Mechanical modeling of the plastic bonded explosive LX17. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-C532.

Council of Science Editors:

Clayton KM. Mechanical modeling of the plastic bonded explosive LX17. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-C532


Texas A&M University

28. Georgie, Jennifer Anne. Selection of desired dynamics for Dynamic Inversion controlled re-entry vehicles.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 Dynamic Inversion is a design technique used to synthesize flight controllers whereby the set of existing plant dynamics are canceled out and replaced by a… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Georgie, J. A. (2012). Selection of desired dynamics for Dynamic Inversion controlled re-entry vehicles. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-G465

Chicago Manual of Style (16th Edition):

Georgie, Jennifer Anne. “Selection of desired dynamics for Dynamic Inversion controlled re-entry vehicles.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-G465.

MLA Handbook (7th Edition):

Georgie, Jennifer Anne. “Selection of desired dynamics for Dynamic Inversion controlled re-entry vehicles.” 2012. Web. 20 Sep 2017.

Vancouver:

Georgie JA. Selection of desired dynamics for Dynamic Inversion controlled re-entry vehicles. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-G465.

Council of Science Editors:

Georgie JA. Selection of desired dynamics for Dynamic Inversion controlled re-entry vehicles. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-G465


Texas A&M University

29. Hoenninger, Corbett Reed. Numerical simulation of the impeller tip clearance effect on centrifugal compressor performance.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 This thesis presents the numerical simulation of flow in centrifugal compressors. A three-dimensional Navier-Stokes solver was employed to simulate flow through two centrifugal compressors. The… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Hoenninger, C. R. (2012). Numerical simulation of the impeller tip clearance effect on centrifugal compressor performance. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-H59

Chicago Manual of Style (16th Edition):

Hoenninger, Corbett Reed. “Numerical simulation of the impeller tip clearance effect on centrifugal compressor performance.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-H59.

MLA Handbook (7th Edition):

Hoenninger, Corbett Reed. “Numerical simulation of the impeller tip clearance effect on centrifugal compressor performance.” 2012. Web. 20 Sep 2017.

Vancouver:

Hoenninger CR. Numerical simulation of the impeller tip clearance effect on centrifugal compressor performance. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-H59.

Council of Science Editors:

Hoenninger CR. Numerical simulation of the impeller tip clearance effect on centrifugal compressor performance. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-H59


Texas A&M University

30. Mayes, John Jeramy. Suitability of Shape Memory Alloys for vibration isolation with application to launch vehicle payloads.

Degree: MS, aerospace engineering, 2012, Texas A&M University

 This work details an investigation into the suitability of Shape Memory Alloys for the task of vibration isolation based on the similarities between the Shape… (more)

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.

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APA (6th Edition):

Mayes, J. J. (2012). Suitability of Shape Memory Alloys for vibration isolation with application to launch vehicle payloads. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-M38433

Chicago Manual of Style (16th Edition):

Mayes, John Jeramy. “Suitability of Shape Memory Alloys for vibration isolation with application to launch vehicle payloads.” 2012. Masters Thesis, Texas A&M University. Accessed September 20, 2017. http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-M38433.

MLA Handbook (7th Edition):

Mayes, John Jeramy. “Suitability of Shape Memory Alloys for vibration isolation with application to launch vehicle payloads.” 2012. Web. 20 Sep 2017.

Vancouver:

Mayes JJ. Suitability of Shape Memory Alloys for vibration isolation with application to launch vehicle payloads. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2017 Sep 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-M38433.

Council of Science Editors:

Mayes JJ. Suitability of Shape Memory Alloys for vibration isolation with application to launch vehicle payloads. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-M38433

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