Wind Tunnel Tests of Ailerons at Various Speeds IV : Ailerons of 0.20 Airfoil Chord and True Contour with 0.35 Aileron-chord Extreme Blunt-nose Balance on the NACA 23012 Airfoil
1943-08-01
Sonstige
Keine Angabe
Englisch
AIRFOILS - NACA 23012 - CHAR & MOMENTS , AILERONS - WIND TUNNEL TESTS , MACH NUMBER , AILERONS, BALANCED - SEALED-GAP , PRESSURE DISTRIBUTION - AIRFOILS - NACA 23012 , FLYING, HIGH-SPEED , CONTROL STICKS - FORCES , LIFT CURVES - SLOPE , WIND TUNNEL TESTS - NACA - STABILITY , AILERONS, BALANCED - HINGE MOMENTS