Transonic viscous-inviscid interaction is considered using the Euler and inverse compressible turbulent boundary-layer equations. Certain improvements in the inverse boundary-layer method are mentioned, along with experiences in using various Runge-Kutta schemes to solve the Euler equations. Numerical conditions imposed on the Euler equations at a surface for viscous-inviscid interaction using the method of equivalent sources are developed, and numerical solutions are presented and compared with experimental data to illustrate essential points
A semi-inverse viscous/inviscid coupling technique for the calculation of compressible flows is pres...
A viscid-inviscid interaction procedure for the calculation of subsonic and transonic flow over a bo...
An explicit multistage Runge-Kutta type of time-stepping scheme is used for solving transonic flow p...
Two different viscous-inviscid interaction schemes have been developed for the analysis of steady tr...
The viscous/inviscid interaction over transonic airfoils with and without suction is studied. The st...
Recent experience in calculating unsteady transonic flow by means of viscous-inviscid interactions w...
An improved method is presented for coupling a boundary layer code with an unsteady inviscid transon...
A method is described for calculating unsteady transonic flow with viscous interaction by coupling a...
A semi-inverse viscous/inviscid coupling technique for the calculation of compressible flows is pres...
The viscous/inviscid interaction over transonic airfoils with and without suction is studied. The st...
Methods for simulating compressible viscous flow using the viscid-inviscid interaction approach are ...
A variety of practical fluid dynamic problems related to the low-speed, high Reynolds number flow ov...
AbstractTo compute transonic flows over a complex 3D aircraft configuration, a viscous/inviscid inte...
The Euler code is used extensively for computation of transonic unsteady aerodynamics. The boundary ...
A streamline Euler solver which combines high accuracy and good convergence rates with capabilities ...
A semi-inverse viscous/inviscid coupling technique for the calculation of compressible flows is pres...
A viscid-inviscid interaction procedure for the calculation of subsonic and transonic flow over a bo...
An explicit multistage Runge-Kutta type of time-stepping scheme is used for solving transonic flow p...
Two different viscous-inviscid interaction schemes have been developed for the analysis of steady tr...
The viscous/inviscid interaction over transonic airfoils with and without suction is studied. The st...
Recent experience in calculating unsteady transonic flow by means of viscous-inviscid interactions w...
An improved method is presented for coupling a boundary layer code with an unsteady inviscid transon...
A method is described for calculating unsteady transonic flow with viscous interaction by coupling a...
A semi-inverse viscous/inviscid coupling technique for the calculation of compressible flows is pres...
The viscous/inviscid interaction over transonic airfoils with and without suction is studied. The st...
Methods for simulating compressible viscous flow using the viscid-inviscid interaction approach are ...
A variety of practical fluid dynamic problems related to the low-speed, high Reynolds number flow ov...
AbstractTo compute transonic flows over a complex 3D aircraft configuration, a viscous/inviscid inte...
The Euler code is used extensively for computation of transonic unsteady aerodynamics. The boundary ...
A streamline Euler solver which combines high accuracy and good convergence rates with capabilities ...
A semi-inverse viscous/inviscid coupling technique for the calculation of compressible flows is pres...
A viscid-inviscid interaction procedure for the calculation of subsonic and transonic flow over a bo...
An explicit multistage Runge-Kutta type of time-stepping scheme is used for solving transonic flow p...