Boundary-layer Transition on a Cooled 20 Degree Cone at Mach Numbers of 1.5 and 2.0
1950-07-01
Miscellaneous
No indication
English
Boundary-layer transition on cooled 20° cone at mach numbers of 1.5 and 2.0
Engineering Index Backfile | 1950
|Boundary layer transition at hypersonic Mach numbers.
NTRS | 1967
|Hypersonic Boundary Layer Transition on a 7 Degree Half-Angle Cone at Mach 10
British Library Conference Proceedings | 2014
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