Proceedings of the Korean Society of Propulsion Engineers Conference (한국추진공학회:학술대회논문집)
- 2003.10a
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- Pages.108-113
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- 2003
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- 1975-342X(pISSN)
Numerical Study of Slot Injection in Supersonic combustor
초음속 연소기내부의 측면제트분사에 대한 수치적 연구
Abstract
The numerical research has been done for the transverse jet behind a rearward- facing step in turbulent supersonic flow without chemical reaction. The purpose of transverse jet is used to improve mixing of the fuel in the combustor. Two- dimensional unsteady flowfields generated by slot injection into supersonic flow are numerically simulated by the integration of Navier-Stokes equation with two-equation k -
Keywords