Numerical simulation of compressible viscous flows around practical aircraft configurations

S. Takanashi, Shigeru Obayashi, K. Matsushima, K. Fujii

Research output: Contribution to conferencePaperpeer-review

Abstract

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.

Original languageEnglish
Publication statusPublished - 1987 Jan 1
Externally publishedYes
Event5th Applied Aerodynamics Conference, 1987 - Monterey , United States
Duration: 1987 Aug 171987 Aug 19

Other

Other5th Applied Aerodynamics Conference, 1987
CountryUnited States
CityMonterey
Period87/8/1787/8/19

ASJC Scopus subject areas

  • Mechanical Engineering
  • Aerospace Engineering

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