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
01.01.1968
Aufsatz (Konferenz)
Keine Angabe
Englisch
Flow phenomena and separation over delta wings with trailing-edge flaps at Mach 6
Engineering Index Backfile | 1968
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