Supersedes NACA -- Tech Note 2264, Jan 1951 indexed in Engineering Index 1951 p 30. (20¢)
Airfoil profiles for minimum pressure drag at supersonic velocities -- General analysis with application to linearized supersonic flow
NACA -- Report
1952
14 pages
Diagrs, Charts
Report
Englisch
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Engineering Index Backfile | 1951
|Supersonic Transitional Airfoil Shapes of Minimum Drag
AIAA | 1997
|