Wind-tunnel Tests of Ailerons at Various Speeds III : Ailerons of 0.20 Airfoil Chord and True Contour with 0.35-aileron-chord Frise Balance on the NACA 23012 Airfoil
1943-09-01
Sonstige
Keine Angabe
Englisch
AILERONS - WIND TUNNEL TESTS , MACH NUMBER , AILERONS - BRISTOL FRISE WIND TUNNEL TESTS (NACA-STABILITY) , PRESSURE DISTRIBUTION - AIRFOILS - NACA 23012 , FLYING, HIGH-SPEED , AIRFOILS - NACA 23012-CHARACTERISTICS , CONTROL STICKS - FORCES , LIFT CURVES - SLOPE , WIND TUNNEL TESTS - NACA - STABILITY , AILERONS, BALANCED - HINGE MOMENTS