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| Author | : United States. National Aeronautics and Space Administration |
| Publisher | : |
| Total Pages | : |
| Release | : 2003* |
| Genre | : |
| ISBN | : |
| Author | : |
| Publisher | : DIANE Publishing |
| Total Pages | : 121 |
| Release | : 2003 |
| Genre | : |
| ISBN | : 1428995145 |
| Author | : |
| Publisher | : |
| Total Pages | : 236 |
| Release | : 1979 |
| Genre | : |
| ISBN | : |
| Author | : George C. Ashby |
| Publisher | : |
| Total Pages | : 82 |
| Release | : 1965 |
| Genre | : Aerodynamics, Hypersonic |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 26 |
| Release | : 1967 |
| Genre | : Aerodynamics, Hypersonic |
| ISBN | : |
| Author | : Robert J. Pegg |
| Publisher | : |
| Total Pages | : 48 |
| Release | : 1962 |
| Genre | : Aerodynamics |
| 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 |
| ISBN | : |
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 | : Manuel Stein |
| Publisher | : |
| Total Pages | : 36 |
| Release | : 1961 |
| Genre | : Mathematical analysis |
| ISBN | : |
| Author | : W. B. Fichter |
| Publisher | : |
| Total Pages | : 28 |
| Release | : 1966 |
| Genre | : Bending |
| ISBN | : |
