Nozzle wall hypersonic boundary layers in helium tunnel, presenting skin friction measurements and heat transfer rates
Nozzle wall boundary layers at Mach numbers 20 to 47
AEROSPACE SCIENCES MEETING ; 1971 ; NEW YORK, NY
1971-01-01
Conference paper
No indication
English
Nozzle Wall Boundary Layers at Mach Numbers 20 to 47
AIAA | 1972
|Nozzle wall boundary layers at Mach numbers 20 to 47
AIAA | 1971
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