Browse > Article
http://dx.doi.org/10.3795/KSME-B.2002.26.3.375

Numerical Simulation of Chemically Reacting Shock Wave-Turbulent Boundary Layer Interactions  

Mun, Su-Yeon (Dept.of Mechanical Engineering, Kyungpook National University)
Lee, Chung-Won (Dept.of Mechanical Engineering, Kyungpook National University)
Son, Chang-Hyeon (Dept.of Mechanical Engineering, Kyungpook National University)
Publication Information
Transactions of the Korean Society of Mechanical Engineers B / v.26, no.3, 2002 , pp. 375-383 More about this Journal
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 (k-$\varepsilon$) model with a compressibility correction. Injection pressures and slot widths are varied in the present study. Pressure, separation extents, and penetration heights are compared with experimental data. Favorable comparisons with experimental measurements are demonstrated.
Keywords
Finite Element Method; Mixing; Reaction; Shock Wave; Generalized Taylor Galerkin;
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
연도 인용수 순위
1 Wilke, C. R., 1950, 'A Viscosity Equation for Gas Mixtures,' J of Chemical Physics, Vol. 18, No. 4   DOI
2 김형문, 이상길, 윤웅섭, 1999, '2차 가스 분사에 의한 원추형 로켓노즐 추력 벡터 제어 성능 해석 (I),' 한국 추진 공학회지, 제3권 제 1호, pp.1-8   과학기술학회마을
3 오대환, 손창현, 이충원, 2000, '2차원 초음속 노즐에서의 2 차 유동 분사에 의한 추력 방향 제어 특성의 수치적 해석,' 한국 추진 공학회지 제 4 권 제 1 호, pp. 13-21   과학기술학회마을
4 Sarkar, S., 1991, 'Application of Reynolds Stress Turbulence Model to the Compressible Shear Layer,' AIAA paper, 91-0523
5 Gordon, S. and McBride, B. J., 1971, Computer Program for Calculation of Complex Chemical Equilibrium Compositions, Rockets Performance, Incident and Reflected Shocks and Chapmann-Jouguet Detonations, NASA SP-273
6 Bird, R. B., 1960, Transport Phenomena, John Wileyand Sons, NewYork
7 White, F. M., 1974, Viscous Fluid Flow, McGraw-Hill
8 StrehlowR. A., 1985, Combustion Fundamentals, McGraw-Hill
9 Yoon, K. T. and Chung, T. J., 1995, 'Unsteady Turbulent Boundary Layer Interactions in High Speed Flows,' AIAA paper 95-2223
10 Moon, S. Y. and Chung, T. J., 1994, 'Airbreathing Combustion in Shock Wave Trubulent Boundary Layer Interactions of High Speed Flows,' AIAA paper, 94-2947
11 Drummon, J. P.and Weidner, E., 1981, 'Numerical Study of a Scramjet Engine Flow Field,' AIAA paper, 81-0186
12 Fujimori, T., Kawai, M., Ikeda, H., Ando, Y., Ohmori, Y., Aso, S. and Fukuda, M., 1991, 'Numerical Prediction of Two-and Three Dimensional Sonic Gas Transverse Injection into Supersonic Flows,' AIAA paper 91-0415
13 Takahashi, M.and Hayashi, A. K., 1991, 'Numerical Study on Mixing and Combustion of Injecting Hydrogen Jet in a Supersonic Air Flow,' AIAA paper, 91-0574
14 Aso, S., Okuyama, S., Kawai, M., and Ando, Y., 1989, 'Experimental Study on Mixing Phenomena in Supersonic Flows with Slot Injection,' AIAA paper 89-1869