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Simplified computation of compressible fluid flow parametersMathematical techniques analyze fluid flow through circular duct, enlarged or constricted circular duct, and across an orifice or nozzle. Using subsonic Mach number as basic flow parameter, a series of working graphs displays the variation of various physical parameters in each of the flow conditions.
Document ID
19700000216
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Beimgraben, H. W. (BOEING CO.)
Date Acquired
August 5, 2013
Publication Date
September 1, 1970
Subject Category
Mechanics
Report/Patent Number
KSC-10400
Report Number: KSC-10400
Accession Number
70B10225
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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