- About
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The Global ETD Search service is a free service for researchers
to find electronic theses and dissertations. This service is
provided by the
Networked Digital Library of Theses and Dissertations.
Our metadata is collected from universities around the world. If you manage a university/consortium/country archive and want to be added, details can be found on the NDLTD website.
Search results
Showing 21 to 30 of 70 (0.143 seconds)Spelling suggestions: "subject:"docket engine."" "subject:"hocket engine.""
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A theoretical study of nonlinear longitudinal combustion instability in liquid propellant rocket enginesLores, Manuel Edward 05 1900 (has links)
No description available.
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| 22 |
Technique for the optimization of the powerhead configuration and performance of liquid rocket enginesSt. Germain, Brad David 08 1900 (has links)
No description available.
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| 23 |
Numerical solution of axial-mode instability problems in solid propellant rocket motorsKooker, Douglas Edward 12 1900 (has links)
No description available.
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| 24 |
A study of clutches for use in a clutchoperated power screw actuator for space applicationsWright, James Glynn 05 1900 (has links)
No description available.
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| 25 |
Numerical simulation of the ejector flowfield in a ram rocket engine with multiple rockets.Kratt, Aaron T. January 2004 (has links)
Thesis (M.A. Sc.)--University of Toronto, 2004. / Adviser: J.P. Sislian.
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| 26 |
Life prediction analysis of a subscale rocket engine combustor using a fluid-thermal-structural modelSarwade, Rohit, Foster, Winfred A. January 2006 (has links) (PDF)
Thesis(M.S.)--Auburn University, 2006. / Abstract. Vita. Includes bibliographic references.
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| 27 |
Spectral modeling of the SSME enhancements and a software system.Bartholomew, David L. January 1992 (has links)
Thesis (M.S.)--Ohio University, August, 1992. / Title from PDF t.p.
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| 28 |
Rayleigh flow of two-phase nitrous oxide as a hybrid rocket nozzle coolant a thesis /Nelson, Lauren, Lemieux, Patrick. January 1900 (has links)
Thesis (M.S.)--California Polytechnic State University, 2009. / Title from PDF title page; viewed on May 26, 2010. Major professor: Patrick Lemieux, Ph.D. "Presented to the faculty of California Polytechnic State University, San Luis Obispo." "In partial fulfillment of the requirements for the degree [of] Master of Science in Mechanical Engineering." "September 2009." Includes bibliographical references (p. 198-201).
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| 29 |
Optimization of a magnetoplasmadynamic arc thrusterKrolak, Matthew Joseph. January 2007 (has links)
Thesis (M.S.) -- Worcester Polytechnic Institute. / Keywords: Electric Propulsion; Plasma thruster; MPD. Includes bibliographical references (leaves 6-13).
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| 30 |
Experimental method of analyzing stress intensity factors and singularity order in rocket motor geometryChe-Way, Chang 16 September 2005 (has links)
A series of frozen stress experiments were conducted on surface flaws of varying aspect ratios in pressurized cylinder with star-shaped cutout in order to study the stress intensity factor distribution along the flaw border and to estimate the loss of the inverse square root singularity when the crack border intersects the inner star surface at right angles. By applying a refined optical method, the photoelastic data are converted into classical stress intensity factors resulting from the three dimensional stress state existing at the inner surface and compared with a numerical analysis to indicate the nearly uniform distribution of the stress intensity factor along the crack border. Based upon this result a two dimensional weight function approach is demonstrated to yield accurate values of the maximum stress intensity factor for the motor grain test geometry. / Ph. D.
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