Supersonic combustion tests with a double- oblique-shock SCRAMjet ina shock tunnel
OSGERBY, I. T., SMITHSON, H. K., WAGNER, D. A. /ARO, INC., ARNOLD AIR FORCE STATION, TENN./.
AIAA Journal ; 8 , 9 ; 1703-1705
1970-01-01
3 pages
Article (Journal)
Electronic Resource
English
INVESTIGATION OF SUPERSONIC COMBUSTION THROUGH MODEL SCRAMJET ENGINE DESIGN AND SHOCK TUNNEL TESTS
British Library Conference Proceedings | 2009
|