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Computer programs for determination of transonic flow parameters in a convergent-divergent nozzlePrograms based on equations that include functions for boundary values along nozzle axis yield different types of flow field configurations. Program's documentation details method of calculating subsonic flow field and sonic line, and describes modified method of characteristics for calculating supersonic flow downstream of sonic line.
Document ID
19700000128
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Jaffe, B.
Rao, G. V. R.
Date Acquired
August 5, 2013
Publication Date
November 1, 1970
Subject Category
Mathematics And Information Sciences
Report/Patent Number
NPO-10895
Report Number: NPO-10895
Accession Number
70B10132
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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