Preliminary measurements in a shock tunnel of shock angle and undersurface pressure to a Nonweiler wing
1963
11 S., [5] Bl.
30 cm
Ill., graph. Darst.
Buch
Englisch
DDC: | 629.13432 |
Scramjet measurements in a shock tunnel
AIAA | 1999
|Preliminary results with a free piston shock tunnel
AIAA | 1965
|