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Axisymmetric reacting gas nonequilibrium performance program

Author
Quan, V.
Published
Oct 1, 1968.
Physical Description
1 electronic document
Additional Creators
Melde, J. E., Kliegel, J. R., and Nickerson, G. R.
Online Version

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Computer program calculates the inviscid one-dimensional equilibrium, frozen, and nonequilibrium nozzle expansion of propellant exhaust mixtures containing these six elements - carbon, hydrogen, oxygen, nitrogen, fluorine, and chlorine plus either aluminum, beryllium, boron or lithium. This program will perform calculations for contoured and conical nozzles.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19680000377.
Accession ID: 68B10377.
MSC-11781.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 16209721