Effects of compressibility on the maximum lift characteristics and spanwise load distribution of a 12-foot-span fighter-type wing of NACA 230-series airfoil sections
1945
13 S., [15] Bl
Ill., graph. Darst
Advance confidential report L5G10
Auch als: Wartime report ; L-51
Report
English
Engineering Index Backfile | 1948
|Engineering Index Backfile | 1947
|