NASA LANGLEY SCIENTIFIC AND TECHNICAL INFORMATION OUTPUT: 1997... NASA/TM-1998-206936... JUL. 6, 1998
Author | : United States. National Aeronautics and Space Administration |
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Total Pages | : |
Release | : 1998* |
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Author | : United States. National Aeronautics and Space Administration |
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Total Pages | : |
Release | : 1998* |
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Author | : George C. Ashby |
Publisher | : |
Total Pages | : 82 |
Release | : 1965 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Author | : George E. Weeks |
Publisher | : |
Total Pages | : 28 |
Release | : 1967 |
Genre | : Buckling (Mechanics) |
ISBN | : |
Author | : James M. Cubbage |
Publisher | : |
Total Pages | : 76 |
Release | : 1971 |
Genre | : Aircraft exhaust emissions |
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Results 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.
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : |
Release | : 1998* |
Genre | : |
ISBN | : |