NASA NTRS · 19910056158
Computational fluid dynamic analysis of liquid rocket combustion instability
Abstract
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.
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Venkateswaran, Sankaran, Grenda, Jeffrey, Merkle, Charles L.. 1991-01-01. Computational fluid dynamic analysis of liquid rocket combustion instability. https://ntrs.nasa.gov/citations/19910056158
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