Computation of Supersonic Flow over Flying Configurations

3

Computation of Axial Disturbance Velocities on Wedged Wings, in Supersonic Flow, at NSL’s Edge

Contents

3.1 General considerations

3.2 The conical flow of first order

3.3 The boundary conditions for the wedged triangular wings, in the Germain’s plane

3.4 The solutions of direct boundary value problems for U and U^* on wedged triangular wing components

3.5 The complex axial disturbance velocities U and U^* on the wedged triangular wing components

3.6 The axial disturbance velocities u and u^* on the wedged delta wing components

3.7 The axial disturbance velocities u and u^* on the wedged trapezoidal wing components

3.8 The axial disturbance velocities u and u^* on the wedged rectangular wing components

3.9 Conclusions

3.1. General considerations ...