Pressure distribution investigation of an NACA 0009 airfoil with a 50 percent chord plain flap and three tabs
pressure-distribution 50-percent-chord
1939
11, [32] Bl.
Miscellaneous
English
RVK: | ZO 7000 |
Engineering Index Backfile | 1939
|Engineering Index Backfile | 1940
|Engineering Index Backfile | 1940
|