Wind tunnel investigation of effect of yaw on lateral-stability characteristics IV : symmetrically tapered wing with a circular fuselage having a wedge-shaped rear and a vertical tail
1942-03-01
Sonstige
Keine Angabe
Englisch
MONOPLANES, MID-WING VS HIGH- & LOW-WING , TAIL SURFACES, VERTICAL , FUSELAGES, CIRCULAR-WEDGE-SHAPED REAR , STABILITY, DIRECTIONAL , WINGS, TAPERED - CHARACTERISTICS EFFECT OF WING FLAPS , WING FLAPS, SPLIT - PARTIAL-SPAN (20% CHORD) , ROLLING & YAWING MOMENTS - AIRFOILS - NACA 23012 , INTERFERENCES - WINGS & FUSELAGES , WINGS - STABILITY, LATERAL