Short duration technique providing simulation of thermodynamic properties and composition of exhaust products of liquid and solid propellant rocket engines
A new technique for simulating rocket engine flow for study of base heating problems.
1966-09-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Numerical Base Heating Sensitivity Study for a Four-Rocket Engine Core Configuration
Online Contents | 2013
|Rocket plume base heating methodology
AIAA | 1993
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