The aerodynamic lift and moment derivatives for pitching oscillations in incompressible flow have been measured for two axis positions on (i) a clipped delta wing of aspect ratio 1.2, (ii) a complete delta wing of aspect ...

Summary.--As a preliminary investigation of the effects of high sweep and low aspect ratio on jet-flap wings, some wind-tunnel experiments were carried out on a half-model of a 60-deg delta wing, already tested with blowing ...

Balance measurements of lift, pitching moment and thrust on an aspect-ratio 6 half-model wing and body in the N.P.L. 13 ft × 9 ft Wind Tunnel are discussed, and compared with theoretical estimates. The experimental ...