Effects of Reynolds Number and Leading-Edge Roughness on Lift and Drag Characteristics of the NACA 653-418, A=1.0 Airfoil Section
1945-11-01
Miscellaneous
No indication
English
Engineering Index Backfile | 1945
|Section characteristics of NACA 0006 airfoil with area suction near leading edge
Engineering Index Backfile | 1954
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