Proceedings of the Korean Society of Propulsion Engineers Conference (한국추진공학회:학술대회논문집)
- 2004.03a
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- Pages.62-68
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- 2004
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- 1975-342X(pISSN)
Dynamic Characteristics of Transverse Fuel Injection and Combustion Flow-Field inside a Scramjet Engine Combustor
Abstract
A comprehensive numerical analysis has been carried out for both non-reacting and reacting flows in a scramjet engine combustor with and without a cavity. The theoretical formulation treats the complete conservation equations of chemically reacting flows with finite-rate chemistry of hydrogen-air. Turbulence closure is achieved by means of a k-
Keywords
- Supersonic Combustion;
- Combustion Instability;
- Air-breathing Propulsion;
- Scramjet Engine;
- Computational Fluid Dynamics