Hypersonic flow distribution and separation types over highly swept delta wings with trailing edge flaps at Mach 6
Flow phenomena and separation over highly swept delta wings with trailing-edge flaps at Mach 6.
AEROSPACE SCIENCES MEETING ; 1968 ; NEW YORK, NY
1968-01-01
Conference paper
No indication
English
Flow phenomena and separation over delta wings with trailing-edge flaps at Mach 6
Engineering Index Backfile | 1968
|Trailing-Edge Flows on Highly-Swept Wings
British Library Conference Proceedings | 1997
|