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Digital holographic diagnostics of aerated-liquid jets in a subsonic crossflowMiller, Brian Derrick, January 2006 (has links) (PDF)
Thesis (M. S.)--Oklahoma State University, 2006. / Vita. Includes bibliographical references.
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Modeling and verification of cryogenic permeability of graphite epoxy laminates with delaminations and stitch cracksNair, Abilash Rajendran. January 2006 (has links) (PDF)
Thesis (M. S.)--Oklahoma State University, 2006. / Vita. Includes bibliographical references.
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Deformation, wave phenomena, and breakup outcomes of round nonturbulent liquid jets in uniform gaseous crossflowNg, Chee-Loon January 2006 (has links) (PDF)
Thesis (Ph. D.)--Oklahoma State University, 2006. / Vita. Includes bibliographical references.
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224 |
Design and safety analysis of an in-flight, test airfoilMcKnight, Christopher William, January 1900 (has links)
Thesis (M. S.)--Texas A&M University, 2006. / "Major Subject: Aerospace Engineering" Title from author supplied metadata (automated record created on Feb. 23, 2007.) Vita. Abstract. Includes bibliographical references.
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The effects of diamond injector angles on flow structures at various Mach numbersMcLellan, Justin Walter, January 1900 (has links)
Thesis (M. S.)--Texas A&M University, 2005. / "Major Subject: Aerospace Engineering" Title from author supplied metadata (automated record created on Feb. 23, 2007.) Vita. Abstract. Includes bibliographical references.
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226 |
Design of fuel optimal maneuvers for multi-spacecraft interferometric imaging systemsRamirez Riberos, Jaime Luis, January 1900 (has links)
Thesis (M. S.)--Texas A&M University, 2006. / "Major Subject: Aerospace Engineering" Title from author supplied metadata (automated record created on Feb. 23, 2007.) Vita. Abstract. Includes bibliographical references.
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227 |
Applications of the thermodynamics of elastic, crystalline materialsSi, Xiuhua, January 1900 (has links)
Thesis (Ph. D.)--Texas A&M University, 2005. / "Major Subject: Aerospace Engineering" Title from author supplied metadata (automated record created on Feb. 23, 2007.) Vita. Abstract. Includes bibliographical references.
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228 |
Applications of Slattery Lagoudas' theory for the stress deformation behavior /Tian, Yongzhe, January 1900 (has links)
Thesis (M. S.)--Texas A&M University, 2005. / "Major Subject: Aerospace Engineering" Title from author supplied metadata (automated record created on Feb. 23, 2007.) Vita. Abstract. Includes bibliographical references.
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229 |
Prevailing Torque Locking Feature Wear-outZimandy, Adam J. C. 10 January 2013
Prevailing Torque Locking Feature Wear-out
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Lard Used as a Fuel for Hybrid Rocket MotorsPfeffer, Daniel Lee 01 May 2007 (has links)
A bio-derived fuel, lard, was successfully tested using a laboratory scale hybrid rocket motor and a static test stand at the University of Tennessee-Knoxville. The experimental setup used gaseous oxygen as the oxidizer. Twenty-three experimental tests were successfully conducted with lard and oxygen. The nine-inch fuel grains used in the current investigation produced a measured thrust ranging from 70-145 Newtons (15-33 pounds) with calculated specific impulses ranging from 122-181 seconds. All the tests conducted were intensely fuel rich, and had equivalence ratios ranging from 0.2 to 0.45. The low equivalence ratios are partially due to unburned fuel particles that exit the nozzle. The tests conducted have shown that the regression rate of the lard was higher than that of other fuels, such as HTPB (hydroxyl-terminated polybutadiene), used in hybrid rocket motors. Lard has produced results similar to those obtained by researchers at Stanford University using paraffin. This investigation has provided sufficient evidence to indicate that lard merits further study as a fuel for hybrid rocket motors.
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