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Quick calculation method for fluid flow through duct systemsConditions for subsonic compressible flow through duct systems are quickly and easily calculated using compact series of curves showing dimensionless parametric functions of Mach number and specific heat ratio. Method is directly applicable to analysis and design of compressible flow systems in industrial fields or processes.
Document ID
19700000469
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Scott, L. R., Jr. (BOEING CO.)
Date Acquired
August 5, 2013
Publication Date
December 1, 1970
Subject Category
Electronic Systems
Report/Patent Number
MFS-15069
Report Number: MFS-15069
Accession Number
70B10487
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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