Numerical simulation of compressible viscous flows around practical aircraft configurations

S. Takanashi; S. Obayashi; K. Matsushima; K. Fujii

Numerical simulation of compressible viscous flows around practical aircraft configurations

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

IFS - Creative Flow Research Division

Research output: Contribution to conference › Paper › peer-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 language	English
Publication status	Published - 1987
Event	5th Applied Aerodynamics Conference, 1987 - Monterey , United States Duration: 1987 Aug 17 → 1987 Aug 19

Conference

Conference	5th Applied Aerodynamics Conference, 1987
Country/Territory	United States
City	Monterey
Period	87/8/17 → 87/8/19

Cite this

@conference{060c208b560e40928a3d10542aa9f3ea,

title = "Numerical simulation of compressible viscous flows around practical aircraft configurations",

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.",

author = "S. Takanashi and S. Obayashi and K. Matsushima and K. Fujii",

note = "Publisher Copyright: {\textcopyright} American Institute of Aeronautics and Astronautics. Inc., 1987. All rights reserved.; 5th Applied Aerodynamics Conference, 1987 ; Conference date: 17-08-1987 Through 19-08-1987",

year = "1987",

language = "English",

}

TY - CONF

T1 - Numerical simulation of compressible viscous flows around practical aircraft configurations

AU - Takanashi, S.

AU - Obayashi, S.

AU - Matsushima, K.

AU - Fujii, K.

PY - 1987

Y1 - 1987

N2 - 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.

AB - 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.

UR - http://www.scopus.com/inward/record.url?scp=85006314497&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=85006314497&partnerID=8YFLogxK

M3 - Paper

AN - SCOPUS:85006314497

T2 - 5th Applied Aerodynamics Conference, 1987

Y2 - 17 August 1987 through 19 August 1987

ER -

Numerical simulation of compressible viscous flows around practical aircraft configurations

Abstract

Conference

Other files and links

Fingerprint

Cite this