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Finite difference simulation of unsteady interactive flowsThe development of time-dependent numerical simulations of unsteady interactive flows of an aerodynamic nature is reviewed with emphasis on compressible flows at flight Reynolds numbers and noniterative schemes based on Navier-Stokes equations. The importance of writing the equations in strong conservation-law form for a generalized body-oriented coordinate system is pointed out. The discussion covers time and length scales and numerical methods currently in use. Some computed results are presented and compared with experimental data.
Document ID
19860036297
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Deiwert, G. S.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Aerodynamics
Accession Number
86A21035
Distribution Limits
Public
Copyright
Other

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