Nose bluntness and cone angle effects on base pressure and heating in laminar hypersonic flow regime, using free flight telemetry technique
Free-flight base pressure and heating measurements on sharp and blunt cones in a shock tunnel.
1967-10-01
Miscellaneous
No indication
English
Shock standoff distances of blunt and sharp cones.
AIAA | 1968
|Free-flight base pressure measurements on 8 deg cones
AIAA | 1978
|