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Numerical simulation of viscous flows over transonic aircraft configurationsNumerical 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.
Document ID
19880016258
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Takanashi, Susumu (National Aerospace Lab. Tokyo (Japan), United States)
Yoshida, Masahiro (National Aerospace Lab. Tokyo (Japan), United States)
Fujii, Kozo (National Aerospace Lab. Tokyo (Japan), United States)
Matsushima, Kisa (Fujitsu Ltd. Tokyo, Japan)
Obayashi, Shigeru (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1987
Publication Information
Publication: National Aerospace Lab., Proceedings of the 5th NAL Symposium on Aircraft Computational Aerodynamics
Subject Category
Aerodynamics
Accession Number
88N25642
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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