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Locating Sonic Lines in Transonic NozzlesNew set of formulas for positions of sonic lines enables more accurate determination of pressures, heat transfers, and flow-discharge coefficients in advanced convergent/divergent nozzles. Older, closedform approximate solutions of Sauer type used to determine best position. In advanced nozzles with shorter transonic fields, such approximations no longer adequate.
Document ID
19870000138
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Wagner, W. R. (Rockwell International Corp.)
Lepore, F. F. (Rockwell International Corp.)
Ostermier, B. J. (Rockwell International Corp.)
Date Acquired
August 13, 2013
Publication Date
March 1, 1987
Publication Information
Publication: NASA Tech Briefs
Volume: 11
Issue: 3
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
MFS-29163
ISSN: 0145-319X
Report Number: MFS-29163
Accession Number
87B10138
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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