NASA NTRS · 19710037947
A single mode approximation in the solution of nonlinear combustion instability problems
Abstract
Unstable liquid propellant rocket engine nonlinear behavior, considering stability of cylindrical combustor with distributed steady state combustion process and multiorifice quasi-steady nozzle
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Powell, E. A., Zinn, B. T.. 1971-01-01. A single mode approximation in the solution of nonlinear combustion instability problems. https://ntrs.nasa.gov/citations/19710037947
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