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http://dx.doi.org/10.6108/KSPE.2020.24.5.065

Aerodynamic Model Development for Three-dimensional Scramjet Model Based on Two-dimensional CFD Analysis  

Han, Song Ee (Department of Aerospace Information Engineering, Konkuk University)
Shin, Ho Cheol (Department of Aerospace Information Engineering, Konkuk University)
Park, Soo Hyung (Department of Mechanical and Aerospace Engineering, Konkuk University)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.24, no.5, 2020 , pp. 65-76 More about this Journal
Abstract
On the initial design process of a scramjet vehicle such as the trajectory prediction, it is inevitable to estimate the aerodynamic performance of a three-dimensional effect. Despite the necessity of intensive computing for the three-dimensional model, it is inefficient in predicting a wide range of aerodynamic performance. In this study, an engineering model for aerodynamic performance was developed based on two-dimensional computational fluid analysis and linearized supersonic inviscid flow theory. Correspondingly, the three-dimension aerodynamic performance relations are presented based on the two-dimensional results. And the additional three-dimensional computation was performed to evaluate the adequacy for the extended relations.
Keywords
Hypersonic Vehicle; Scramjet Engine; CFD; Aerodynamic Model;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
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1 Kim, K.H., Kim, C. and Rho, O.H., "Methods for the accurate computations of hypersonic flows: I. AUSMPW+ scheme," Journal of Computational Physics, Vol. 174, No. 1, pp. 38-80, 2001.   DOI
2 Murthy, S.N.B. and Curran, E.T., Scramjet propulsion, American Institute of Aeronautics and Astronautics, Reston, Virginia, U.S.A., 2001.
3 Curran, E.T., "Scramjet engines: the first forty years," Journal of Propulsion and Power, Vol. 17, No. 6, pp. 1138-1148, 2001.   DOI
4 Engelund, W.C., Holland, S.D., Cockrell, Jr C.E. and Bittner, R.D., "Aerodynamic database development for the hyper-X airframe-integrated scramjet propulsion experiments," Journal of Spacecraft and Rockets, Vol. 38, No. 6, pp. 803-810, 2001.   DOI
5 Buning, P.G., Wong, T.C., Dilley, A.D. and Pao, J.L., "Computational fluid dynamics prediction of hyper-x stage separation aerodynamics," Journal of Spacecraft and Rockets, Vol. 38, No. 6, pp. 820-827, 2001.   DOI
6 Won S.H., Jeong, I.S. and Kim, J.S., "Overview on hypersonic scramjet engine developments," Journal of the Korean Society of Propulsion Engineers, Vol. 9, No. 1, pp. 67-83, 2005.
7 Ha, J.H., Das, R., Ladeinde, F., Kim, T.H. and Kim H.D., "Numerical study on mode transition in a scramjet engine," Journal of the Korean Society of Propulsion Engineers, Vol. 21, No. 6, pp. 21-31, 2017.
8 Park, S.H. and Kwon, J.H., "Implementation of k-ω turbulence models in an implicit multigrid method," AIAA journal, Vol. 42, No. 7, pp. 1348-1357, 2004.   DOI
9 Roe, P.L., "Approximate Riemann solvers, parameter vectors, and difference schemes," Journal of computational physics, Vol. 43, No. 2, pp. 357-372, 1981.   DOI
10 Liou, M.S., "A sequel to AUSM: AUSM+," Journal of computational physics, Vol. 129, No. 2, pp. 364-382, 1996.   DOI
11 Sung, C.H., Park, S.H. and Kwon, J.H., "Multigrid Diagonalized-ADI method for compressible flows," 15th AIAA Computational Fluid Dynamics Conference, pp. 2556, 2001.
12 Anderson, J.D., Fundamentals of aerodynamics, 5th ed., McGraw-Hill Education, New York, N.Y., U.S.A., 2010.
13 Bailey, A.B., and Hiatt, J., "Sphere drag coefficients for a broad range of Mach and Reynolds numbers," AiAA Journal, Vol. 10, No. 11, pp. 1436-1440, 1972.   DOI
14 Lee, K.J, Kang, S.H., Yang, S.S. and Park, C., "Conceptual design study of two-stage hypersonic scramjet vehicle," Journal of the Korean Society of Propulsion Engineers, Vol. 16, No. 1, pp. 16-24, 2012.   DOI
15 Tan, H.J., Sun, S. and Yin, Z.L., "Oscillatory flows of rectangular hypersonic inlet unstart caused by downstream mass-flow choking," Journal of Propulsion and Power, Vol. 25, No. 1, pp. 138-147, 2009.   DOI