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Solutions of Transonic Flow in TurbomachinesAccurate approximation obtained using perturbation techniques. Pertubation procedures determine highly accurate approximations to families of nonlinear solutions either continuous or discontinuous and represent variations in some arbitrary parameter. Program written in FORTRAN IV.
Document ID
19830000186
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Stahara, S. (Nielson Engineering & Research, Inc.)
Elliott, J. (Nielson Engineering & Research, Inc.)
Spretter, J. (Nielson Engineering & Research, Inc.)
Date Acquired
August 11, 2013
Publication Date
October 1, 1983
Publication Information
Publication: NASA Tech Briefs
Volume: 7
Issue: 4
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LEW-13896
Accession Number
83B10186
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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