Add to ORKGThe use of a fast elliptic solver in combination with relaxation is presented as an effective way to accelerate the convergence of transonic flow calculations, particularly when a marching scheme can be used to treat the supersonic zone in the relaxation process
Solving of test problems with the TRANDES program is discussed. This method utilizes the full, invis...
A program, XTRAN2L, for solving the general-frequency unsteady transonic small disturbance potential...
A two-step semidirect procedure is developed to accelerate the one-step procedure described in NASA ...
A technique is described for the efficient numerical solution of nonlinear partial differential equa...
A method is presented for the calculation of in viscid, supercritical flowfields about axisymmetric ...
Numerical techniques that improve the accuracy and stability of algorithms for the small disturbance...
This paper report progress on a technique to accelerate the convergence to steady solutions when the...
Spectral multigrid methods are demonstrated to be a competitive technique for solving the transonic ...
A multi-level grid method was studied as a possible means of accelerating convergence in relaxation ...
An explicit method for solving the transonic small-disturbance potential equation is presented. This...
A finite element method for the computation of the transonic flow with shocks past airfoils is prese...
Implicit approximate factorization techniques (AF) were investigated for the solution of matrix equa...
Perturbation procedures and associated computational codes for determining nonlinear flow solutions ...
The finite element method is applied for the solution of transonic potential flows through a cascade...
Studies on applications of the finite element approach to transonic flow calculations are reported. ...
Solving of test problems with the TRANDES program is discussed. This method utilizes the full, invis...
A program, XTRAN2L, for solving the general-frequency unsteady transonic small disturbance potential...
A two-step semidirect procedure is developed to accelerate the one-step procedure described in NASA ...
A technique is described for the efficient numerical solution of nonlinear partial differential equa...
A method is presented for the calculation of in viscid, supercritical flowfields about axisymmetric ...
Numerical techniques that improve the accuracy and stability of algorithms for the small disturbance...
This paper report progress on a technique to accelerate the convergence to steady solutions when the...
Spectral multigrid methods are demonstrated to be a competitive technique for solving the transonic ...
A multi-level grid method was studied as a possible means of accelerating convergence in relaxation ...
An explicit method for solving the transonic small-disturbance potential equation is presented. This...
A finite element method for the computation of the transonic flow with shocks past airfoils is prese...
Implicit approximate factorization techniques (AF) were investigated for the solution of matrix equa...
Perturbation procedures and associated computational codes for determining nonlinear flow solutions ...
The finite element method is applied for the solution of transonic potential flows through a cascade...
Studies on applications of the finite element approach to transonic flow calculations are reported. ...
Solving of test problems with the TRANDES program is discussed. This method utilizes the full, invis...
A program, XTRAN2L, for solving the general-frequency unsteady transonic small disturbance potential...
A two-step semidirect procedure is developed to accelerate the one-step procedure described in NASA ...