Convergence of Two Analytical Flowfield Models Predicting a Destabilizing Agent in Rocket Combustion
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چکیده
منابع مشابه
Convergence of Two Analytical Flowfield Models Predicting a Destabilizing Agent in Rocket Combustion
In the combustion stability assessment of solid propellant rocket motors, several new destabilizing terms are introduced when rotational-flow effects are properly accounted for. Such effects must be included when the wave motion is parallel to the burning surface. A normal fluctuating velocity component then appears in a careful resolution of intrinsic fluid dynamics, including acoustico–vortic...
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ژورنال
عنوان ژورنال: Journal of Propulsion and Power
سال: 2000
ISSN: 0748-4658,1533-3876
DOI: 10.2514/2.5595