Numerical simulation of compressible viscous flow fields is performed for a transonic transport configuration. A single structured grid system is constructed using analytical transformations such as conformal mapping, shearing/twisting/rotating/clustering/stretching transformations. The Reynolds-averaged, thin-layer Navier-Stokes equations are solved on a supercomputer, FACOM VP-400, using the LU-ADI factorization method.
Numerical simulation of viscous flows over transonic aircraft configurations
1987-11-01
Conference paper
No indication
English
Numerical simulation of viscous transonic airfoil flows
AIAA | 1987
|Transonic Aircraft Configurations
AIAA | 2012
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