Hydrocarbon-Fueled Scramjet Research at Hypersonic Mach Numbers
Final rept. 1 Feb 2002-31 Mar 2003
AUSTRALIAN NATIONAL UNIV CANBERRA DEPTOF PHYSICS
Pagination or Media Count:
Planar laser-induced fluorescence PLIF of OH and wall-pressure measurements have been used to investigate the combustion in a cavity flame-holder scramjet combuster.
- Jet and Gas Turbine Engines