NASA NTRS · 19700000216
Simplified computation of compressible fluid flow parameters
Abstract
Mathematical 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.
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Beimgraben, H. W.. 1970-09-01. Simplified computation of compressible fluid flow parameters. https://ntrs.nasa.gov/citations/19700000216
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