Unsteady Combustion in Gaseous Propellant Rocket Motors
PRINCETON UNIV NJ DEPT OF AEROSPACE AND MECHANICAL SCIENCES
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This research work was directed toward the development of a consistent experimental and theoretical description of the phenomenon of intrinsic unstable combustion in the gas rocket. A determination was achieved of the contribution of gas phase rate processes, in particular, chemical kinetics , to the coupling of a finite-dimensional unsteady turbulent combustion zone and finite amplitude linear and nonlinear longitudinal mode pressure oscillations.
- Combustion and Ignition
- Rocket Propellants