Boundary-layer Transition at Mach 3.12 as Affected by Cooling and Nose Blunting
1957-01-01
Miscellaneous
No indication
English
Boundary-layer transition at mach 3.12 as affected by cooling and nose blunting
Engineering Index Backfile | 1957
|Study of boundary-layer transition and surface temperature distributions at mach 3.12
Engineering Index Backfile | 1955
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