Studies of Airframe-propulsion-system Integration for Mach 6 Cruise Vehicles
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Published: 1967
Total Pages: 26
ISBN-13:
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Author:
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Published: 1967
Total Pages: 26
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DOWNLOAD EBOOKAuthor: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
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Published: 1968
Total Pages: 428
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DOWNLOAD EBOOKAuthor: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
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Published: 1968
Total Pages: 436
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Published: 1994
Total Pages: 1038
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Published: 1967-10
Total Pages: 1020
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Published: 1967
Total Pages: 590
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Published: 1978
Total Pages: 106
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DOWNLOAD EBOOKAuthor: James M. Cubbage
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Published: 1971
Total Pages: 76
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DOWNLOAD EBOOKResults from an investigation of the effects of underexpanded engine exhaust flow on the aerodynamic performance and stability of a cruise airplane at Mach 6 are presented. The influence of wing reflex angle and nozzle geometry on exhaust flow interference effects was investigated on a flat-plate model. The experiments were conducted at a free-stream Reynolds number of 17.05 X 10 (to the 6 power) based on the length of the airplane model over a model angle-of-attack range of 0(degrees) to 10(degrees) and at nozzle static-pressure ratios from 1 to approximately 4.
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Published: 1992
Total Pages: 176
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