Wind-tunnel investigation of effect of yaw on lateral-stability characteristics V : symmetrically tapered wing with a circular fuselage having a horizontal and a vertical tail
1943-06-01
Sonstige
Keine Angabe
Englisch
FUSELAGES, CIRCULAR , TAIL SURFACES, VERTICAL , WINGS - DIHEDRAL & SWEEPBACK , TAIL SURFACES - END PLATES , WINGS, TAPERED - CHARACTERISTICS EFFECT OF WING FLAPS , ROLLING & YAWING MOMENTS - AIRFOILS - NACA 23012 , STABILITY, LATERAL , WING FLAPS, SPLIT - PARTIAL-SPAN (20%-CHORD) , WINGS - STABILITY, LATERAL , TAIL SURFACES, HORIZONTAL - WIND TUNNEL TESTS