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Texas A&M University
1. Colling, James David. Sailplane glide performance and control using fixed and articulating winglets.
Degree: MS, aerospace, 2012, Texas A&M University
URL: http://hdl.handle.net/1969.1/ETD-TAMU-1995-THESIS-C65
Subjects/Keywords: aerospace.; Major aerospace.
Record Details
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APA (6th Edition):
Colling, J. D. (2012). Sailplane glide performance and control using fixed and articulating winglets. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1995-THESIS-C65
Chicago Manual of Style (16th Edition):
Colling, James David. “Sailplane glide performance and control using fixed and articulating winglets.” 2012. Masters Thesis, Texas A&M University. Accessed February 27, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-1995-THESIS-C65.
MLA Handbook (7th Edition):
Colling, James David. “Sailplane glide performance and control using fixed and articulating winglets.” 2012. Web. 27 Feb 2021.
Vancouver:
Colling JD. Sailplane glide performance and control using fixed and articulating winglets. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 27]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1995-THESIS-C65.
Council of Science Editors:
Colling JD. Sailplane glide performance and control using fixed and articulating winglets. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1995-THESIS-C65
Texas A&M University
2. 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
URL: http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-K563
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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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 February 27, 2021. 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. 27 Feb 2021.
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 2021 Feb 27]. 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
3. Kinser Robert Eric. Development of neural network calibration algorithms for multi-port pressure probes.
Degree: MS, aerospace engineering, 2012, Texas A&M University
URL: http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-K57
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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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 February 27, 2021. 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. 27 Feb 2021.
Vancouver:
Eric KR. Development of neural network calibration algorithms for multi-port pressure probes. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 27]. 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
4. McCann, Barrett Taylor. Evaluation of local preconditioners for multigrid solutions of the compressible Euler equations.
Degree: MS, aerospace engineering, 2012, Texas A&M University
URL: http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-M326
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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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 February 27, 2021. 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. 27 Feb 2021.
Vancouver:
McCann BT. Evaluation of local preconditioners for multigrid solutions of the compressible Euler equations. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 27]. 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
5. Mani, Somnath. A reduced Blade-Vortex Interaction rotor.
Degree: MS, aerospace engineering, 2012, Texas A&M University
URL: http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-M362
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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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 February 27, 2021. 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. 27 Feb 2021.
Vancouver:
Mani S. A reduced Blade-Vortex Interaction rotor. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 27]. 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
6. 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
URL: http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-N47
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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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 February 27, 2021. 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. 27 Feb 2021.
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 2021 Feb 27]. 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
7. Pisor, Robert Donald. Design and analysis of large deformation spiral springs.
Degree: MS, aerospace engineering, 2012, Texas A&M University
URL: http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-P57
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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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 February 27, 2021. 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. 27 Feb 2021.
Vancouver:
Pisor RD. Design and analysis of large deformation spiral springs. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 27]. 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
8. Sundstrom, Keith Andrew. Stress analysis of a hybrid composite drilling riser.
Degree: MS, aerospace engineering, 2012, Texas A&M University
URL: http://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-S87
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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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 February 27, 2021. 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. 27 Feb 2021.
Vancouver:
Sundstrom KA. Stress analysis of a hybrid composite drilling riser. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 27]. 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
9. 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
URL: http://hdl.handle.net/1969.1/ETD-TAMU-1997-THESIS-D37
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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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 February 27, 2021. 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. 27 Feb 2021.
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 2021 Feb 27]. 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
10. 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
URL: http://hdl.handle.net/1969.1/ETD-TAMU-1997-THESIS-F68
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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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 February 27, 2021. 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. 27 Feb 2021.
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 2021 Feb 27]. 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
11. Gilliatt, Heather Colleen. Investigations of internal resonance phenomena and related nonlinear pathologies in aeroelastic systems.
Degree: MS, aerospace engineering, 2012, Texas A&M University
URL: http://hdl.handle.net/1969.1/ETD-TAMU-1997-THESIS-G534
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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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 February 27, 2021. 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. 27 Feb 2021.
Vancouver:
Gilliatt HC. Investigations of internal resonance phenomena and related nonlinear pathologies in aeroelastic systems. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 27]. 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
12. 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
URL: http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-G55
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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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 February 27, 2021. 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. 27 Feb 2021.
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 2021 Feb 27]. 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
13. Honea, Mark Stephen. An analysis of electrothermodynamic heating and cooling.
Degree: MS, aerospace engineering, 2012, Texas A&M University
URL: http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-H66
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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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 February 27, 2021. 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. 27 Feb 2021.
Vancouver:
Honea MS. An analysis of electrothermodynamic heating and cooling. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 27]. 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
14. Huang, Haiming. Identification and control of a flexible structure.
Degree: MS, aerospace engineering, 2012, Texas A&M University
URL: http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-H825
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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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 February 27, 2021. 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. 27 Feb 2021.
Vancouver:
Huang H. Identification and control of a flexible structure. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 27]. 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
15. Johansen, Espen S. Steady and unsteady calibration of multi-hole probes.
Degree: MS, aerospace engineering, 2012, Texas A&M University
URL: http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-J63
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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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 February 27, 2021. 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. 27 Feb 2021.
Vancouver:
Johansen ES. Steady and unsteady calibration of multi-hole probes. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 27]. 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
16. 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
URL: http://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-J863
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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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 February 27, 2021. 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. 27 Feb 2021.
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 2021 Feb 27]. 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
17. Collard, Joseph Eugene. Blade-forced vibration effects in turbomachinery rotor-stator interaction.
Degree: MS, aerospace engineering, 2012, Texas A&M University
URL: http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-C625
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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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 February 27, 2021. 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. 27 Feb 2021.
Vancouver:
Collard JE. Blade-forced vibration effects in turbomachinery rotor-stator interaction. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 27]. 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
18. 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
URL: http://hdl.handle.net/1969.1/ETD-TAMU-1994-THESIS-D158
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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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 February 27, 2021. 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. 27 Feb 2021.
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 2021 Feb 27]. 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
19. 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
URL: http://hdl.handle.net/1969.1/ETD-TAMU-1994-THESIS-D273
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
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 February 27, 2021. 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. 27 Feb 2021.
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 2021 Feb 27]. 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
20. 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
URL: http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-O79
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
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 February 27, 2021. 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. 27 Feb 2021.
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 2021 Feb 27]. 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
21. Rao, Preetham P. Active flow separation control using synthetic jet actuators.
Degree: MS, aerospace engineering, 2012, Texas A&M University
URL: http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-R37
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
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 February 27, 2021. 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. 27 Feb 2021.
Vancouver:
Rao PP. Active flow separation control using synthetic jet actuators. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 27]. 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
22. 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
URL: http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-S24
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
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 February 27, 2021. 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. 27 Feb 2021.
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 2021 Feb 27]. 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
23. Smith, David Matthew. Agility metric sensitivity using linear error theory.
Degree: MS, aerospace engineering, 2012, Texas A&M University
URL: http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-S613
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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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 February 27, 2021. 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. 27 Feb 2021.
Vancouver:
Smith DM. Agility metric sensitivity using linear error theory. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 27]. 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
24. Wilkins, Matthew Paul. Characterizing orbit uncertainty due to atmospheric uncertainty.
Degree: MS, aerospace engineering, 2012, Texas A&M University
URL: http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-W343
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
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 February 27, 2021. 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. 27 Feb 2021.
Vancouver:
Wilkins MP. Characterizing orbit uncertainty due to atmospheric uncertainty. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 27]. 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
25. Wilson, Larry Nixon. Development of a shape memory alloy actuated biomimetic hydrofoil.
Degree: MS, aerospace engineering, 2012, Texas A&M University
URL: http://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-W36
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
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 February 27, 2021. 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. 27 Feb 2021.
Vancouver:
Wilson LN. Development of a shape memory alloy actuated biomimetic hydrofoil. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 27]. 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
26. Alonso, Roberto Jorge. Relative navigation for formation flying of spacecraft.
Degree: MS, aerospace engineering, 2012, Texas A&M University
URL: http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-A453
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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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 February 27, 2021. 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. 27 Feb 2021.
Vancouver:
Alonso RJ. Relative navigation for formation flying of spacecraft. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 27]. 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
27. Bryson, Amy Louise. Optimal command generation for maneuvering the space station.
Degree: MS, aerospace engineering, 2012, Texas A&M University
URL: http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-B79
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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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 February 27, 2021. 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. 27 Feb 2021.
Vancouver:
Bryson AL. Optimal command generation for maneuvering the space station. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 27]. 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
28. Clayton, Kyle Martin. Mechanical modeling of the plastic bonded explosive LX17.
Degree: MS, aerospace engineering, 2012, Texas A&M University
URL: http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-C532
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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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 February 27, 2021. 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. 27 Feb 2021.
Vancouver:
Clayton KM. Mechanical modeling of the plastic bonded explosive LX17. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 27]. 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
29. Georgie, Jennifer Anne. Selection of desired dynamics for Dynamic Inversion controlled re-entry vehicles.
Degree: MS, aerospace engineering, 2012, Texas A&M University
URL: http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-G465
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
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 February 27, 2021. 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. 27 Feb 2021.
Vancouver:
Georgie JA. Selection of desired dynamics for Dynamic Inversion controlled re-entry vehicles. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 27]. 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
30. Hoenninger, Corbett Reed. Numerical simulation of the impeller tip clearance effect on centrifugal compressor performance.
Degree: MS, aerospace engineering, 2012, Texas A&M University
URL: http://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-H59
Subjects/Keywords: aerospace engineering.; Major aerospace engineering.
Record Details
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
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 February 27, 2021. 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. 27 Feb 2021.
Vancouver:
Hoenninger CR. Numerical simulation of the impeller tip clearance effect on centrifugal compressor performance. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 27]. 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