Acknowledgement
본 연구는 방위사업청 국방과학연구소 연구사업(UE191011GD, UD210034SD)의 지원으로 수행되었습니다. 이에 대해 감사드립니다.
References
- Heo, Y., Moon, G. H. and Sung, H. G., "Investigation of Oswatisch Scheme for Maximum Total Pressure Recovery of Hypersonic Wedge-type Intakes," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 45, No. 12, 2017, pp. 2287~6871.
- Cox, C., Lewis, R., Pap, R., Glover, C., Priddy, K., Edwards, J., McCarty, C. and Wagner, E., "Prediction of Unstart Phenomena in Hypersonic Aircraft," AIAA Journal, Vol. 6, April 1995, pp. 3~7. https://doi.org/10.2514/3.55361
- Juntao, C., Nan, L., Kejing, X., Wen, B. and Daren, Y., "Recent research progress on unstart mechanism, detection and control of hypersonic inlet," Progress in Aerospace Sciences, Vol. 89, 2017, pp. 1~22. https://doi.org/10.1016/j.paerosci.2016.12.001
- Wilcox, D. C., Turbulence Modeling for CFD, 2ed Ed., DCW Industry, California, 2002, pp. 171~203.
- Sung, H. G., Kim, S. J., Yeom, H. Y. and Heo, J. Y., "On the Assessment of Compressibility Effects of Two-Equation Turbulence Models for Supersonic Transition Flow with Flow Separation," International Journal of Aeronautical and Space Science, Vol. 14, 2013, pp. 387~397. https://doi.org/10.5139/IJASS.2013.14.4.387
- Menter, F. R., Kuntz, M. and Langtry, R., "Ten Years Industrial Experience with the SST Turbulence Model," Turbulence Heat and Transfer, Vol. 4, 2003, pp. 625~632.
- Kim, J. C. and Sung, H. G., "Aerospace Problem Solving through Modular Multiphysics 3-D CFD code development," Proceedings of the Korea Society of Propulsion Engineers Spring Conference, Vol. 56, May 2021, pp. 203~206.
- Kitamura, K. and Hashimoto, A., "Reduced dissipation AUSM-family fluxes: HR-SLAU2 amd HR-AUSM+-up for high resolution unsteady flow simulations," Computers and Fluids, Vol. 126, 2016, pp. 41~57. https://doi.org/10.1016/j.compfluid.2015.11.014
- Schulein, E., "Development and Application of the thin of Flim Technique for Skin Friction Measurements in the Short Duration Hypersonic Wind Tunnel," AIAA Journal, Vol. 1, 2004, pp. 334~338. https://doi.org/10.2514/3.1533
- Manan, A. V. and David, F., "Mach 5 shock wave boundary layer interaction," NASA www.grc.nass.gov/WWW/windvalid/m5swbli/m5swbli.html, 2011.
- Wagner, J. L., Yuceil, K. B., Valdivia, A., Clemens, N. T. and Dolling, D. S., "Experimental Investigation of Unstart in an Inlet/Isolator Model in Mach 5 Flow," AIAA Journal, Vol. 47, 2009, pp. 1528~1542. https://doi.org/10.2514/1.40966
- Koo, H. S. and Venkatramanan, R. R., "Large-Eddy Simulation of a Supersonic Inlet-Isolator," AIAA Journal, Vol. 7, 2012, pp. 1596~1613.