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Navier-Stokes simulation of wind-tunnel flow using LU-ADI factorization algorithmThe three dimensional Navier-Stokes solution code using the LU-ADI factorization algorithm was employed to simulate the workshop test cases of transonic flow past a wing model in a wind tunnel and in free air. The effect of the tunnel walls is well demonstrated by the present simulations. An Amdahl 1200 supercomputer having 128 Mbytes main memory was used for these computations.
Document ID
19880008200
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Obayashi, Shigeru
(NASA Ames Research Center Moffett Field, CA., United States)
Fujii, Kozo
(NASA Ames Research Center Moffett Field, CA., United States)
Gavali, Sharad
(Amdahl Corp. Sunnyvale, Calif., United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1988
Subject Category
Aerodynamics
Report/Patent Number
A-88027
NAS 1.15:100042
NASA-TM-100042
Report Number: A-88027
Report Number: NAS 1.15:100042
Report Number: NASA-TM-100042
Accession Number
88N17584
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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