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
|