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Numerical program for analysis of three-dimensional supersonic exhaust flow fields (CHAR 3D)Choice of reference plane orientation depends on specific nozzle geometry, with different configurations requiring different reference plane systems. In addition, for given configuration several reference systems may be used in different regions of flow field, so each system is locally aligned with flow.
Document ID
19740000236
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Dash, S. (Advanced Technol. Labs., Inc.)
Guidice, P. D. (Advanced Technol. Labs., Inc.)
Ferri, A. (Advanced Technol. Labs., Inc.)
Roffe, G. (Advanced Technol. Labs., Inc.)
Date Acquired
August 7, 2013
Publication Date
December 1, 1974
Subject Category
Mathematics And Information Sciences
Report/Patent Number
LAR-11596
Report Number: LAR-11596
Accession Number
74B10236
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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