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Interactive computer graphics applications for compressible aerodynamicsThree computer applications have been developed to solve inviscid compressible fluids problems using interactive computer graphics. The first application is a compressible flow calculator which solves for isentropic flow, normal shocks, and oblique shocks or centered expansions produced by two dimensional ramps. The second application couples the solutions generated by the first application to a more graphical presentation of the results to produce a desk top simulator of three compressible flow problems: 1) flow past a single compression ramp; 2) flow past two ramps in series; and 3) flow past two opposed ramps. The third application extends the results of the second to produce a design tool which solves for the flow through supersonic external or mixed compression inlets. The applications were originally developed to run on SGI or IBM workstations running GL graphics. They are currently being extended to solve additional types of flow problems and modified to operate on any X-based workstation.
Document ID
19950010849
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Benson, Thomas J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1994
Subject Category
Computer Programming And Software
Report/Patent Number
AIAA PAPER 95-0119
E-9279
NASA-TM-106802
NAS 1.15:106802
Report Number: AIAA PAPER 95-0119
Report Number: E-9279
Report Number: NASA-TM-106802
Report Number: NAS 1.15:106802
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Reno, NV
Country: United States
Start Date: January 9, 1995
End Date: January 12, 1995
Accession Number
95N17264
Funding Number(s)
PROJECT: RTOP 505-62-52
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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