The paper presents a computational analysis of liquid rocket combustion instability. Consideration is given to both a fully nonlinear unsteady calculation as well as a new CFD-based linearized stability analysis. An analytical solution for the linear stability problem in a constant area combustion chamber with uniform mean flow is developed to verify the numerical analyses.
Computational fluid dynamic analysis of liquid rocket combustion instability
AIAA Computational Fluid Dynamics Conference ; 1991 ; Honolulu, HI, United States
1991-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Liquid propellant rocket combustion instability
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