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Supersonic combustion ramjet enginesShowing 1 featured edition. View all 1 editions?
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Investigation of a 2-D scramjet inlet, M =8-25 and T =800-4, 100K
1991, American Institute of Aeronautics and Astronautics
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Book Details
Edition Notes
Includes bibliographical references: p. 10-11.
Source: AIAA Third International Aerospace Planes Conference, 3-5 December 1991/Orlando, Fl
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- Created October 21, 2008
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