Wind-tunnel Investigation at High and Low Subsonic Mach Numbers of Two Unswept Wings Having NACA 2-006 and NACA 65A006 Airfoil Sections
1953-12-04
Miscellaneous
No indication
English
Aerodynamic effects caused by icing of unswept NACA 65A004 airfoil
Engineering Index Backfile | 1958
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