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Streamline curvature design procedure for subsonic and transonic ductsA procedure for designing ducts for subsonic and transonic speeds is described. Examples discussed are a wind-tunnel contraction cone, a supersonic nozzle, and a diffuser. A listing of the computer program is included. The streamline curvature equations represent a form of the exact, compressible, inviscid flow equations. The method is applicable from low subsonic to supersonic speeds.
Document ID
19740003705
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Barger, R. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1973
Subject Category
Aerodynamics
Report/Patent Number
L-8963
NASA-TN-D-7368
Report Number: L-8963
Report Number: NASA-TN-D-7368
Accession Number
74N11818
Funding Number(s)
PROJECT: RTOP 501-06-09-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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