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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 138 (0.032 seconds)Spelling suggestions: "subject:"pockets"" "subject:"sockets""
| 21 |
Experimental determination of three-dimensional liquid rocket nozzle admittancesBell, William Alvin 08 1900 (has links)
No description available.
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| 22 |
The effect of nozzle nonlinearities on the nonlinear stability of liquid rocket motorsPadmanabhan, Mysore Srikantiah 12 1900 (has links)
No description available.
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| 23 |
The effect of departure from ideality of a multiply ionized monatomic gas on the performance of rocket engines /Perkins, John Noble, January 1963 (has links)
Thesis (Ph. D.)--Virginia Polytechnic Institute, 1963. / Vita. Abstract. Includes bibliographical references (leaves 54-56). Also available via the Internet.
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| 24 |
Thermal stresses in a finite solid-propellant grain /Frohlich, Jurgen Paul, January 1962 (has links)
Thesis (M.S.)--Virginia Polytechnic Institute, 1962. / Vita. Abstract. Includes bibliographical references (leaf 59). Also available via the Internet.
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| 25 |
The interaction between throttling and thrust vectoring of an annular aerospike nozzle a thesis /Imbaratto, David, Murray, William Russell. January 1900 (has links)
Thesis (M.S.)--California Polytechnic State University, 2009. / Mode of access: Internet. Title from PDF title page; viewed on September 23, 2009. Major professor: William R. Murray. "Presented to the faculty of the College of Engineering, 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. 80).
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| 26 |
Wake closure conditions in plug nozzle flowfields /Lang, Derek Edward. January 1999 (has links)
Thesis (Ph. D.)--University of Washington, 1999. / Vita. Includes bibliographical references (leaves 132-140).
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| 27 |
Hole-type aerospike compound nozzle thrust vectoring a thesis /Beebe, Stanley Ikuo. Murray, William Russell. January 1900 (has links)
Thesis (M.S.)--California Polytechnic State University, 2009. / Mode of access: Internet. Title from PDF title page; viewed on September 28, 2009. Major professor: William Murray, Ph.D. "Presented to the faculty of California Polytechnic State University, San Luis Obispo." "In partial fulfillment of the requirement for the degree [of] Master of Science in Mechanical Engineering." "September 2009." Includes bibliographical references (p. 49-50).
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| 28 |
Impact of ion propulsion on performance, design, testing and operation of a geosynchronous spacecraftLugtu, Spotrizano Descanzo. January 1990 (has links)
Thesis (M.S. in Astronautical Engineering)--Naval Postgraduate School, June 1990. / Thesis Advisor(s): Agrawal, Brij N. Second Reader: Biblarz, Oscar. "June 2009." Description based on title screen as viewed on 19 October 2009. DTIC Identifier(s): Ion propulsion, synchronous satellites, NSSK (North South Station Keeping). Author(s) subject terms: Ion propulsion, geosynchronous satellite, North-South Station Keeping. Includes bibliographical references (p. 153-156). Also available in print.
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| 29 |
Performance of a solid propellent rocket /Yassin, Jamal Saleh. January 1986 (has links)
Thesis (M.S.)--Ohio State University, 1986. / Includes bibliographical references (leaf 77).
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| 30 |
Helium plasma jet : construction and plasma properties.Morris, Robert Norton January 1968 (has links)
A model - of which a similar type was found applicable to an argon plasma jet - is developed and applied to a laminar helium jet operated at atmospheric pressure with a current of 185 amps. The results are used to investigate the equilibrium properties of the plasma. It was found that the helium plasma was not in a state of Local Thermodynamic Equilibrium but that the neutral atoms were considerably
colder than the electrons. (Te ≈ 17,000°K; To≈5,700°K)
Instructions are given in the thesis on the construction, operation and properties of a d.c. plasma jet. / Science, Faculty of / Physics and Astronomy, Department of / Graduate
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