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Software For Analyzing Performances Of Wind TunnelsSubsonic Wind Tunnel Performance Analysis computer program developed as aid in design and analysis of subsonic wind tunnels. Brings together and refines previously scattered and oversimplified techniques used for design of, and prediction of losses in, components of subsonic wind tunnels. Implements system of equations for determining total pressure losses and provides general guidelines for design of diffusers, contractions, corners, and inlets and exits of nonreturn tunnels. Written in FORTRAN and BASIC.
Document ID
19930000122
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Decker, C.
(NASA Ames Research Center, Moffett Field, CA.)
Date Acquired
August 16, 2013
Publication Date
March 1, 1993
Publication Information
Publication: NASA Tech Briefs
Volume: 17
Issue: 3
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
ARC-13129
ISSN: 0145-319X
Report Number: ARC-13129
Accession Number
93B10122
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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