A wind-tunnel investigation was conducted to determine the effect of wing planform on sonic boom at Mach numbers of 1.7, 2.0, and 2.7. The results of the investigation show that the wing leading-edge sweep is one of the primary planform variables affecting the overpressure characteristics.
Some Effects of Wing Planform on Sonic Boom
1973-01-01
Miscellaneous
No indication
English
Some Effects of Wing Planform on Sonic Boom
NTIS | 1973
|Some effects of wing planform on sonic boom
TIBKAT | 1973
|NTRS | 1973
|NTIS | 1973
|