Pressure distributions and force tests of an NACA 65-210 airfoil section with a 50-percent-chord flap
1946
7 S., [31] Bl
graph. Darst
Book
English
Pressure distributions and force tests of NACA 65-120 airfoil section with 50-percent-chord flap
Engineering Index Backfile | 1947
|Engineering Index Backfile | 1947
|