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Computing Jet-Exhaust/Crossflow InteractionsJETPLT and JETBOD programs developed to predict velocity and pressure induced by subsonic jets exhausting into subsonic free stream. JETPLT predicts pressures induced on infinite flat plate by jet exhausting at angles to plate. JETBOD, in conjunction with panel code, predicts pressures induced on body of revolution by jet exhausting perpendicularly to surface. Programs used to investigate interactions between jet exhausts and crossflows in vertical/short-takeoff-andlanding aircraft shifting from hover to forward flight, where inducedpressure loading leads to reduction in lift. JETPLT/JETBOD written in FORTRAN 77.
Document ID
19870000079
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Perkins, S. C., Jr.
(Nielsen Engineering and Research, Inc.)
Mendenhall, M.
(Nielsen Engineering and Research, Inc.)
Date Acquired
August 13, 2013
Publication Date
February 1, 1987
Publication Information
Publication: NASA Tech Briefs
Volume: 11
Issue: 2
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
ARC-11597
Accession Number
87B10079
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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