Results are presented for wind tunnel tests at M(infinity) = 3.51 on four wings with pointed vertices and sharp leadlng edges. Two conical models were tested through a wide range of angles of incidence and yaw and the ...
The first order solution of the problem of the supersonic flow past a flat elliptic cone set symmetrically to the wind indicates that the pressure over the surface is constant if the body lies within the Mach cone of the ...