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
1969-01-01
3 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Nozzle Wall Boundary Layers at Mach Numbers 20 to 47
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