Proceedings of the KSME Conference (대한기계학회:학술대회논문집)
- 2001.11b
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- Pages.475-480
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- 2001
Numerical Simulation of Mixing and Combustion in a Normal Injection of the Scramjet
초음속 연소기에서의 혼합과 연소현상에 관한 수치해석
- Published : 2001.11.01
Abstract
The flowfield of transverse jet in a supersonic air stream subjected to shock wave turbulent boundary layer interactions is simulated numerically by Generalized Taylor Galerkin(GTG) finite element methods. Effects of turbulence are taken into account with a two-equation
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