An investigation was conducted to determine the magnitude of the groundtrack overpressure generated by an oblique-wing transport cruising at Mach 1.4 at 45,000 ft. A conventional swept-wing configuration was included in the study to provide a basis of comparison for the oblique-wing configuration. The results of the investigation have shown that the oblique-wing configuration produces less sonic boom overpressure at cruise lift coefficient than the swept-wing vehicle.
Oblique-wing sonic boom
1973-02-01
Report
Keine Angabe
Englisch
Sonic boom of the oblique flying wing
AIAA | 1994
|Sonic Boom of the Oblique Flying Wing
Online Contents | 1994
|The Sonic Boom of an Oblique Flying Wing
British Library Conference Proceedings | 1995
|The sonic boom of an oblique flying wing
AIAA | 1990
|