A study has been performed to determine the optimum, practical high-energy driver technique to be employed with the Air Force Aero Propulsion Laboratory 120-inch shock tunnel. The aerodynamic performance and engineering design and feasibility of several candidate techniques were investigated. (Author)
Study of Large, High - Performance Shock Tunnel Drivers
1967
83 pages
Report
No indication
English
Laboratory & Test Facility Design & Operation , Shock tubes , Performance(Engineering) , Shock(Mechanics) , Underground structures , Supersonic combustion , Supersonic combustion ramjet engines , Aerodynamics , Helium , Hydrogen , Simulation , Velocity , Hydrostatic pressure , Heaters , O-rings , Diaphragms(Mechanics) , Shock tunnel drivers
Hypersonic Shock Tunnel Performance Characteristics
NTIS | 1974
|Shock Tunnel Investigation of Scramjet Performance
British Library Conference Proceedings | 1996
|