Flow phenomena and separation over delta wings with trailing-edge flaps at Mach 6.
KEYES, J. W. /NASA, LANGLEY RESEARCH CENTER, HAMPTON, VA./., WHITEHEAD, A. H., JR.
AIAA Journal ; 6 , 12 ; 2380-2387
1968
Article (Journal)
Electronic Resource
English
Flow phenomena and separation over delta wings with trailing-edge flaps at Mach 6
Engineering Index Backfile | 1968
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