Investigation at a Mach Number of 1.2 of Two 45 Degree Sweptback Wings Utilizing NACA 2-006 and NACA 65A006 Airfoil Sections
1952-09-11
Miscellaneous
No indication
English
Theoretical and experimental data for number of NACA 6A-series airfoil sections
Engineering Index Backfile | 1947
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