Nozzle boundary-layer displacement thickness at Mach numbers 30 to 70
MILLER, C. G. /NASA, LANGLEY RESEARCH CENTER, AERO-PHYSICS DIV., HAMPTON, VA./.
AIAA Journal ; 7 , 11 ; 2165-2167
1969
Article (Journal)
Electronic Resource
English
Boundary-layer displacement effects in air at mach numbers of 6.8 and 9.6
Engineering Index Backfile | 1959
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