Pressure-distribution Data for the NACA 64(sub 1)-012 and 64(sub 1) A012 Airfoils at High Subsonic Mach Numbers
1949-05-06
Miscellaneous
No indication
English
Transition at Low-Re Numbers for UAV Type Airfoils at High Subsonic Mach Numbers
British Library Conference Proceedings | 2012
|Engineering Index Backfile | 1959
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