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Interim user's manual for boundary layer integral matrix procedure, version JA computer program for analyzing two dimensional and axisymmetric nozzle performance with a variety of wall boundary conditions is described. The program has been developed for application to rocket nozzle problems. Several aids to usage of the program and two auxiliary subroutines are provided. Some features of the output are described and three sample cases are included.
Document ID
19740020643
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Evans, R. M. (Aerotherm Corp. Mountain View, CA, United States)
Morse, H. L. (Aerotherm Corp. Mountain View, CA, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1974
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-120268
AEROTHERM-UM-74-41
Report Number: NASA-CR-120268
Report Number: AEROTHERM-UM-74-41
Accession Number
74N28756
Funding Number(s)
CONTRACT_GRANT: NAS8-29667
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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