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A method for simulating 3-D aircraft flow fields with jet plume effectsThe objective is to develop, demonstrate, and document a coupled flow analysis procedure for computing 3D aircraft flow fields with deflected subsonic and supersonic jet exhaust plumes. The PNS plume code was transferred to the Ames computer facility for execution on the Cray computer. No problems were encountered when installing this code. The Bower's test case is currently being run. This case is being used to fine tune the procedure for coupling the plume code to PANAIR.
Document ID
19850018353
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 5, 2013
Publication Date
January 1, 1984
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:175802
MTPR-15
NASA-CR-175802
Report Number: NAS 1.26:175802
Report Number: MTPR-15
Report Number: NASA-CR-175802
Accession Number
85N26664
Funding Number(s)
CONTRACT_GRANT: NAS2-11711
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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