Preliminary Data on the Effect of Body-nose Bluntness on the Drag and Pressure Recovery of a Side-inlet-body Combination at Mach Numbers of 1.4 and 1.7
1951-04-25
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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