NASA NTRS · 19700068309
Nonlinear combustion instability in liquid- propellant rocket engines
Abstract
Liquid propellant rocket engine combustion instabilities, describing unsteady combustor flow by single nonlinear wave equation with stable and unstable finite amplitude limit cycles
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Powell, E. A., Zinn, B. T.. 1970-08-01. Nonlinear combustion instability in liquid- propellant rocket engines. https://ntrs.nasa.gov/citations/19700068309
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