다음과 같은 기능을 한번의 로그인으로 사용 할 수 있습니다.
NTIS 바로가기
한국추진공학회지 = Journal of the Korean Society of Propulsion Engineers, v.25 no.6, 2021년, pp.36 - 44
김재은 (Department of Aerospace Engineering, Pusan National University) , 정승민 (Department of Aerospace Engineering, Pusan National University) , 최정열 (Department of Aerospace Engineering, Pusan National University) , 황유준 (Agency for Defense Development)
AI-Helper
Numerical analysis was performed on the shock wave-boundary layer interaction generated in the internal flow path of the curved interstage of the scramjet engine flight test vehicle. For numerical analysis, the turbulence model k-ω SST was used in the compressibility Raynolds Averaged Navier ...
Hank, J. M., Murphy, J. S. and Mutzman, R. C., "The X-51A scramjet engine flight demonstration program," 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, Ohio, pp. 2540, Apr. 2008.
Curran, E. T. and Murthy, S. N. B., Scramjet propulsion, AIAA, 2001.
Choi, J. Y., Jeung, I. S. and Yoon, Y. B., "Computational fluid dynamics algorithms for unsteady shock-induced combustion, part 1: validation," AIAA, Vol. 38, No. 7, pp. 1179-1187, 2000.
Roe, P. L., "Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes," Journal of Computational Physics, Vol. 43, pp. 357-372, 1981.
Harten, A., "High resolution schemes for hyperbolic conservation laws," Journal of Computational Physics, Vol. 135, No. 2, pp. 260-278, 1997.
Wagner, J. L., "Experimental studies of unstart dynamics in inlet/isolator configurations in a Mach 5 flow," Ph.D. Dissertation, Aerospace Engineering and Engineering Mechanics, The University of Texas at Austin, 2009.
Jang, I., Pecnik, R. and Moin, P., "A numerical study of the unstart event in an inlet/isolator model," Center for Turbulence Research Annual Research Briefs, pp. 93-103, 2010.
Koo, H. S. and Raman, V., "Large-eddy simulation of a supersonic inlet-isolator," AIAA, Vol. 50, No. 7, pp. 1596-1613, 2012.
Settles, G. S., Fitzparpick, T. J. and Bogdonoff, S. M., "Detailed study of attached and separated compression corner flowfields in high Reynolds number supersonic flow," AIAA, Vol. 17, No. 6, pp. 579-585, 1979.
Clemens, N. T. and Venkateswaran, N., "Low-frequency unsteadiness of shock wave/turbulent boundary layer interactions," Annual Review of Fluid Mechanics, Vol. 46, pp. 469-492, 2014.
Mears, L. J., Baldwin, A., Ali, M. Y. and Kumar, R., "Spatially resolved mean and unsteady surface pressure in swept SBLI using PSP," Experiments in Fluids, Vol. 61, No. 4, pp. 1-14, 2020.
Gao, X., Xiang, G. X., Tang, W. J., Jie, X. Z., Huang, X. He, J. Y. and Liu, S. A., "Investigations on the complex flows induced by dual-swept/dual-ramp wedges in supersonic flows," Scientific Reports, Vol. 10, No.1, pp. 1-9, 2020.
*원문 PDF 파일 및 링크정보가 존재하지 않을 경우 KISTI DDS 시스템에서 제공하는 원문복사서비스를 사용할 수 있습니다.
오픈액세스 학술지에 출판된 논문
Copyright KISTI. All Rights Reserved.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.