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
25.04.1951
Sonstige
Keine Angabe
Englisch
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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