Force and pressure measurements on several canopy- fuselage configurations at low supersonic speeds
FORCE AND PRESSURE MEASUREMENTS ON SEVERAL CANOPY-FUSELAGE CONFIGURATIONS AT MACH NUMBERS 1.41 AND 2.01
1955-12-15
Miscellaneous
No indication
English
Effect of nose bluntness on transition for cone and hollow cylinder at Mach numbers 1.41 and 2.01
Engineering Index Backfile | 1961
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