A parametric simulation of compressible viscous flow fields is carried out for an advanced transonic transport configuration under development. A single grid system for the computation is constructed by the sequential use of analytical transformations. The Reynolds averaged Navier Stokes equations in a thin-layer form are solved on a supercomputer, FACOM VP 400, using the LL-ADI factorization technique. Some of the computed results are presented which show good agreement with the wind tunnel test data.
|Publication status||Published - 1987|
|Event||5th Applied Aerodynamics Conference, 1987 - Monterey , United States|
Duration: 1987 Aug 17 → 1987 Aug 19
|Conference||5th Applied Aerodynamics Conference, 1987|
|Period||87/8/17 → 87/8/19|