Add to ORKGFirst-and second-order numerical procedures are presented for calculating two-dimensional transonic flows that treat shock waves as discontinuities. Their application to a simple but nontrivial problem for which there are limited theoretical results is discussed
A formulation of the lambda scheme for the analysis of two dimensional inviscid, compressible, unste...
The stream function equation in conservation form is solved iteratively based on the artificial comp...
Solving of test problems with the TRANDES program is discussed. This method utilizes the full, invis...
The numerical solution of a single, mixed, nonlinear equation with prescribed boundary data is discu...
A Lagrangian method is developed to solve the Euler equations of gas dynamics. The solution of the e...
The study illustrates the possible advantages of using shock fitting techniques to solve transonic a...
A development was the time linearization of the density function. This linearization reduces the sol...
A highly accurate approximation and a rapidly convergent numerical procedure are developed for two d...
A finite difference procedure based upon a system of unsteady equations in proper conservation form ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76375/1/AIAA-9312-844.pd
A fast computer program was developed to eliminate the shocks by slightly altering portions of the c...
Two transonic computational schemes which are based on the Integral Equation Formulation of the full...
A finite element method for the computation of the transonic flow with shocks past airfoils is prese...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76259/1/AIAA-1985-369-965.pd
The problem of inviscid, steady transonic conical flow, formulated in terms of the small disturbance...
A formulation of the lambda scheme for the analysis of two dimensional inviscid, compressible, unste...
The stream function equation in conservation form is solved iteratively based on the artificial comp...
Solving of test problems with the TRANDES program is discussed. This method utilizes the full, invis...
The numerical solution of a single, mixed, nonlinear equation with prescribed boundary data is discu...
A Lagrangian method is developed to solve the Euler equations of gas dynamics. The solution of the e...
The study illustrates the possible advantages of using shock fitting techniques to solve transonic a...
A development was the time linearization of the density function. This linearization reduces the sol...
A highly accurate approximation and a rapidly convergent numerical procedure are developed for two d...
A finite difference procedure based upon a system of unsteady equations in proper conservation form ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76375/1/AIAA-9312-844.pd
A fast computer program was developed to eliminate the shocks by slightly altering portions of the c...
Two transonic computational schemes which are based on the Integral Equation Formulation of the full...
A finite element method for the computation of the transonic flow with shocks past airfoils is prese...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76259/1/AIAA-1985-369-965.pd
The problem of inviscid, steady transonic conical flow, formulated in terms of the small disturbance...
A formulation of the lambda scheme for the analysis of two dimensional inviscid, compressible, unste...
The stream function equation in conservation form is solved iteratively based on the artificial comp...
Solving of test problems with the TRANDES program is discussed. This method utilizes the full, invis...