Boundary-layer Transition at Mach 3.12 as Affected by Cooling and Nose Blunting
01.01.1957
Sonstige
Keine Angabe
Englisch
Boundary-layer transition at mach 3.12 as affected by cooling and nose blunting
Engineering Index Backfile | 1957
|Boundary-layer transition at Mach 3.12 with and without single roughness elements
Engineering Index Backfile | 1954
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