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Axisymmetric two-phase perfect gas performance programComputer program calculates the inviscid axisymmetric nozzle expansion of propellant systems having both gaseous and condensed exhaust products. The program uses velocity and thermal lags and will perform calculations for contoured and conical nozzles.
Document ID
19680000374
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Kliegel, J. R.
Nickerson, G. R.
Date Acquired
August 4, 2013
Publication Date
October 1, 1968
Subject Category
Mathematics And Information Sciences
Report/Patent Number
MSC-11774
Report Number: MSC-11774
Accession Number
68B10374
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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