About this document
Combustion Instability in Rocket Engines by AR Bangash is a document available to read on EtoBox.
This technical report describes a nonlinear model for analyzing liquid rocket engine combustion instability. The model combines a steady-state vaporization model with a nonlinear instability model. It allows engineers to determine zones in a rocket engine chamber where high frequency instability is most likely to initiate. The report details the steady-state vaporization model for monopropellants like monomethylhydrazine and the nonlinear instability model. It also includes the computer programs used to imp
- Author
- AR Bangash
- Language
- EN