A relaxation method is described for the numerical solution of the transonic small disturbance equation for flow about a slender body of revolution. Results for

Summary: Approximate solutions of the nonlinear equations of the small disturbance theory of transonic flow are found for the pressure distribution on pointed s

An analytical solution is obtained for the perturbation velocity potential for transonic flow about lifting wing-body configurations with order-one span-length

Theoretical analysis and associated computer programs were developed for predicting properties of transonic flows about certain classes of wing-body combination