Studies of Airframe-propulsion-system Integration for Mach 6 Cruise Vehicles
Title | Studies of Airframe-propulsion-system Integration for Mach 6 Cruise Vehicles PDF eBook |
Author | |
Publisher | |
Pages | 26 |
Release | 1967 |
Genre | Aerodynamics, Hypersonic |
ISBN |
NASA Technical Note
Title | NASA Technical Note PDF eBook |
Author | |
Publisher | |
Pages | 586 |
Release | 1976 |
Genre | |
ISBN |
NASA Scientific and Technical Reports
Title | NASA Scientific and Technical Reports PDF eBook |
Author | United States. National Aeronautics and Space Administration Scientific and Technical Information Division |
Publisher | |
Pages | 428 |
Release | 1968 |
Genre | Aeronautics |
ISBN |
A Selected Listing of NASA Scientific and Technical Reports
Title | A Selected Listing of NASA Scientific and Technical Reports PDF eBook |
Author | United States. National Aeronautics and Space Administration. Scientific and Technical Information Division |
Publisher | |
Pages | 436 |
Release | 1968 |
Genre | Aeronautics |
ISBN |
Scientific and Technical Aerospace Reports
Title | Scientific and Technical Aerospace Reports PDF eBook |
Author | |
Publisher | |
Pages | 1038 |
Release | 1994 |
Genre | Aeronautics |
ISBN |
Investigation of Engine-exhaust-airframe Interference on a Cruise Vehicle at Mach 6
Title | Investigation of Engine-exhaust-airframe Interference on a Cruise Vehicle at Mach 6 PDF eBook |
Author | James M. Cubbage |
Publisher | |
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.
Government-wide Index to Federal Research & Development Reports
Title | Government-wide Index to Federal Research & Development Reports PDF eBook |
Author | |
Publisher | |
Pages | 1020 |
Release | 1967-10 |
Genre | Government publications |
ISBN |