Boundary-layer transition at Mach 3.12 with and without single roughness elements.
Boundary-layer transition at Mach 3.12 with and without single roughness elements
NACA -- Tech Note
1954
41 pages
Report
Englisch
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Study of boundary-layer transition and surface temperature distributions at mach 3.12
Engineering Index Backfile | 1955
|Boundary-layer transition at mach 3.12 as affected by cooling and nose blunting
Engineering Index Backfile | 1957
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