Add to ORKGA relaxation method is described for the numerical solution of the transonic small disturbance equation for flow about a slender body of revolution. Results for parabolic arc bodies, both with and without an attached sting, are compared with wind-tunnel measurements for a free-stream Mach number range from 0.90 to 1.20. The method is also used to show the effects of wind-tunnel wall interference by including boundary conditions representing porous-wall and open-jet wind-tunnel test sections
The time-dependent Transonic Small Disturbance equation, will be reformulated in Hyperbolic Conser...
The object of this research is to examine two particular problems of transonic flow. The first probl...
A finite difference procedure based upon a system of unsteady equations in proper conservation form ...
A relaxation method is described for the numerical solution of the transonic small disturbance equat...
Approximate solutions of the nonlinear equations of the small disturbance theory of transonic flow a...
The three-dimensional problem of transonic flow about lifting wing-body configurations is reduced to...
Results computed by a finite-difference, relaxation algorithm are presented for the supercritical fl...
The local linearization method for axisymmetric flow is combined with the transonic equivalence rule...
Procedures based on the method of local linearization and transonic equivalence rule were developed ...
The purpose of this report is to provide a detailed and comprehensive account of a transonic approxi...
A method is presented for the approximate solution of the nonlinear equations transonic flow theory....
A multi-level grid method was studied as a possible means of accelerating convergence in relaxation ...
Sonic flow past a non-lifting, slender body of revolution is investigated by the use of small distur...
The problem of inviscid, steady transonic conical flow, formulated in terms of the small disturbance...
The unsteady transonic small disturbance equation for an oscillating slender body is obtained from t...
The time-dependent Transonic Small Disturbance equation, will be reformulated in Hyperbolic Conser...
The object of this research is to examine two particular problems of transonic flow. The first probl...
A finite difference procedure based upon a system of unsteady equations in proper conservation form ...
A relaxation method is described for the numerical solution of the transonic small disturbance equat...
Approximate solutions of the nonlinear equations of the small disturbance theory of transonic flow a...
The three-dimensional problem of transonic flow about lifting wing-body configurations is reduced to...
Results computed by a finite-difference, relaxation algorithm are presented for the supercritical fl...
The local linearization method for axisymmetric flow is combined with the transonic equivalence rule...
Procedures based on the method of local linearization and transonic equivalence rule were developed ...
The purpose of this report is to provide a detailed and comprehensive account of a transonic approxi...
A method is presented for the approximate solution of the nonlinear equations transonic flow theory....
A multi-level grid method was studied as a possible means of accelerating convergence in relaxation ...
Sonic flow past a non-lifting, slender body of revolution is investigated by the use of small distur...
The problem of inviscid, steady transonic conical flow, formulated in terms of the small disturbance...
The unsteady transonic small disturbance equation for an oscillating slender body is obtained from t...
The time-dependent Transonic Small Disturbance equation, will be reformulated in Hyperbolic Conser...
The object of this research is to examine two particular problems of transonic flow. The first probl...
A finite difference procedure based upon a system of unsteady equations in proper conservation form ...