Wind-tunnel tests of ailerons at various speeds ; 4: Ailerons of 0.20 airfoil chord and true contour with 0.35 aileron-chord extreme blunt-nose balance on the NACA 23012 airfoil
Wartime report ; L-433
1943
17 S., [30] Bl
Ill., graph. Darst
Originally issued August 1943 as Advance confidential report 3H28
Buch
Englisch