Computation of Supersonic Flow over Flying Configurations

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Computation of Axial Disturbance Velocities on Flying Configurations with Arbitrary Shapes, in Supersonic Flow, at NSL’s Edge

Contents

4.1 General considerations

4.2 The theory of high conical flow of nth order

4.3 The principle of minimal singularities for the high conical flow of nth order

4.4 The solutions of boundary value problems of fictitious complex potentials F_f and F_f^*, on triangular wings

4.5 The axial disturbance velocities on the thin and thick-symmetrical triangular wings with arbitrary shapes

4.6 The axial disturbance velocities on delta wings with arbitrary shapes

4.7 The axial disturbance velocities on trapezoidal wings with arbitrary shapes

4.8 The axial disturbance velocities on rectangular wings with arbitrary shapes ...