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PROGRAM VSAERO: A computer program for calculating the non-linear aerodynamic characteristics of arbitrary configurations: User's manualVSAERO is a computer program used to predict the nonlinear aerodynamic characteristics of arbitrary three-dimensional configurations in subsonic flow. Nonlinear effects of vortex separation and vortex surface interaction are treated in an iterative wake-shape calculation procedure, while the effects of viscosity are treated in an iterative loop coupling potential-flow and integral boundary-layer calculations. The program employs a surface singularity panel method using quadrilateral panels on which doublet and source singularities are distributed in a piecewise constant form. This user's manual provides a brief overview of the mathematical model, instructions for configuration modeling and a description of the input and output data. A listing of a sample case is included.
Document ID
19850006493
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Maskew, B.
(Analytical Methods, Inc. Bellevue, WA, United States)
Date Acquired
September 5, 2013
Publication Date
December 1, 1982
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-166476
NAS 1.26:166476
Report Number: NASA-CR-166476
Report Number: NAS 1.26:166476
Accession Number
85N14802
Funding Number(s)
PROJECT: RTOP 505-31-21
CONTRACT_GRANT: NAS2-8788
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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