subject:(Aerospace)

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

► An experimental study was conducted to investigate the effects of controllable articulating winglets on glide performance and yawing moments of high performance sailplanes. Testing was… (more)

▼ An experimental study was conducted to investigate the effects of controllable articulating winglets on glide performance and yawing moments of high performance sailplanes. Testing was conducted in the Texas A&M University 7xlO foot Low Speed Wind Tunnel using a full-scale model of the outboard 5.6 feet of a 15 meter class high performance sailplane wing. Different wing tip configurations could be easily mounted to the wing model. A winglet was designed in which the cant and toe angles as well as a rudder on the winglet could be adjusted to a range of positions. Cant angles used in the investigation consisted of 5, 25, and 40 degrees measured from the vertical axis. Toe-out angles ranged from 0 to 22.5 degrees. A rudder on the winglet was used to study the effects of changing the camber of the winglet airfoil on wing performance and wing yawing moments. Rudder deflections consisted of -10, 0, and 10 degrees. Test results for a fixed geometry winglet and a standard wing tip are presented to show the general behavior of winglets on sallplane wings, and the effects of boundary- layer turbulators on the winglets are also presented. By tripping the laminar boundary-layer to turbulent before laminar separation occurs, the wing performance was increased at low Reynolds numbers. The effects on the lift and drag, yawing moment, pitching moment, and wing root bending moment of the model are presented. Oil flows were used on the wing model with the fixed geometry winglet and the standard wing tip to visualize flow directions and areas of boundary layer transition. A cant angle of 25 degrees and a toe-out angle of 2.5 degrees provided an optimal increase in wing performance for the cant and toe angles tested. Maximum performance was obtained when the winglet rudder remained in the neutral position of zero degrees. By varying the cant, toe, and rudder angles from their optimized positions, wing performance decreases. Although the winglet rudder proved to be more effective in increasing the yawing moment compared to varying the cant and toe angles, the amount of increased yawing moment was insignificant when compared to that produced by the vertical tail. A rudder on the winglet was determined to be ineffective for providing additional yaw control.

Subjects/Keywords: aerospace.; Major aerospace.

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APA (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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)

▼ 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 mean wake dynamic pressure measurements around two wavy cylinders of differing wavelength at a Reynolds number which produces laminar separation (ReD= 100,000), one producing turbulent separation (ReD= 400,000), and one transitional Reynolds number (ReD= 200,000). These tests revealed that similar characteristics exist between flow fields involving laminar and turbulent separation. The attachment line flow, and the existence of a highly three dimensional separation were characteristics found at all Reynolds numbers tested. Always characteristic of the separation were separation singularities which, at all Reynolds numbers tested, abnormally narrowed the near wake behind geometric nodes. Though these general flow characteristics were present at all Reynolds numbers tested, many other wavy cylinder flow field characteristics were found to change with a transition from laminar to turbulent separation. A state of turbulent separation caused the separation line to move downstream, greatly reducing secondary separation effects, and narrowing the wake. Movement of the separation line was small enough to indicate that its location was insensitive to the state of the boundary layer. The singularities, however, were more sensitive to the state of the boundary layer just prior to separation. The change to turbulent separation on the wavy cylinder was also found to add enough vorticity to the singularities through axial stretching to allow them to significantly influence surface flow well into the separated region of the cylinder. Not only was the separated region affected by singularities, but in some cases increased coherency of the singularities allowed them to influence the far wake as well. The far wake behind cylinder B (X/D = 2.4) was influenced by singularities which were coherent enough to withstand dissipation by the strain field in the wake. This was not the case with cylinder E (X/D = 1.2) where higher rates of model curvature caused large lateral strain fields in the wake which were capable of rapidly dissipating coherent singularities at all Reynolds numbers tested.

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

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APA (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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)

▼ 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 various types of errors and uncertainties is not understood. This research effort develops a framework for analyzing the sensitivity of agility metrics to initial condition errors, structured parametric uncertainties, and coordinate system type without the need to resort to time consuming and costly Monte Carlo analysis. Linear error theory is used to quantify the sensitivity of a selected set of agility metrics, and the results are then verified with both time histories and traditional Monte Carlo methods. The four selected metrics are time to roll through bank angle metric, time-averaged integral of pitch rate metric, power onset/loss parameter metric, and the Combat Cycle Time metric. Results show that the time to roll through bank angle metric is weakly nonlinear to initial condition errors and parametric uncertainties. The time-averaged integral of pitch rate metric is linear to initial condition error in pitch rate. The power onset/loss parameter metrics are strongly nonlinear to initial condition errors and parametric uncertainties, and the Combat Cycle Time metric is also strongly nonlinear to initial condition errors and parametric uncertainties. Using the Beck metrics expressed in the Frenet coordinate system, the time to roll through bank angle metric is more sensitive to initial condition errors and parametric uncertainties than when expressed in the Cartesian coordinate system. The time-averaged integral of pitch rate and power onset/loss parameter metrics were less sensitive to initial condition errors and parametric uncertainties when expressed using the Beck metrics than when expressed in the Cartesian coordinate system. The Combat Cycle Time metric results indicate little difference between the sensitivity of the metrics to coordinate system type. Finally, the linear error theory method for analyzing the sensitivity of agility metrics has been verified.

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

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APA (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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 (6^th 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 (16^th 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 (7^th 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

► 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.

Record Details Similar Records Cite « Share

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

APA (6^th 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 (16^th 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 (7^th 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

► 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.

Record Details Similar Records Cite « Share

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

APA (6^th 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 (16^th 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 (7^th 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

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