Wind-tunnel tests of ailerons at various speeds ; 1: Ailerons of 0.20 airfoil chord and true contour with 0.35 aileron-chord extreme blunt nose balance on the NACA 66,2-216 airfoil
Wartime report ; L-431
1943
13 S., [31] Bl
Ill., graph. Darst
Originally issued June 1943 as Advance confidential report 3F11
Buch
Englisch