과제정보
본 논문은 방위사업청과 국방과학연구소로부터 지원받은 '복합영역 경계층 제어기술'과제의 연구 결과물입니다.
참고문헌
- Lee, Y.J., Kang, S.H., Oh, J.H. and Yang, S.S., "Development of the Scramjet engine Test Facility(SeTF) in Korea Aerospace Research Institute," Journal of the Korean Society of Propulsion Engineers, Vol. 14, No. 3, pp. 69-78, 2010.
- Kang, S.H., Lee, Y.J. and Yang, S.S., "Experimental Study of a Scramjet Engine Intake in a Storage Heater Type Hypersonic Wind Tunnel," 2010 KSPE Fall Conference Proceeding, Jeju, Korea, pp. 463-466, Nov. 2010.
- Lee, Y.J., Kang, S.H. and Yang, S.S., "Starting Characteristics Study of Scramjet Engine Test Facility(SETF)," Journal of the Korean Society of Propulsion Engineers, Vol. 15, No. 2, pp. 15-22, 2011.
- Yang, I.Y., Lee, Y.J., Lee, K.J. and Kim, Y.M., "Intake Start Characteristics of a Mach 5 Scramjet Engine," 2012 KSPE Spring Conference Proceeding, Gumi, Korea, pp. 1-4, May 2012.
- Grunnet, J.L. and Laster, M.L., "Pressure Recovery in Hypersonic Engine Test Facilities," J. Spacecraft, Vol. 4, No. 5, pp. 643-649, 1967. https://doi.org/10.2514/3.28922
- Lee, Y.J., Yang, I.Y. and Yang, S.S., "A Starting Characteristics Study of the Scramjet Engine Test Facility with a Mach 5.0 Nozzle," Journal of the Korean Society of Propulsion Engineers, Vol. 17, No. 4 pp. 63-72, 2013. https://doi.org/10.6108/KSPE.2013.17.4.063
- Mitani, T., Hiraiwa, T., Kanda, T., Shimura, T., Tomioka, S., Kobayashi, K., Izumikawa, M., Sakuranaka, N., Watanabe, S., Tarukawa, Y., Kouchi, T., Kitamura, E. and Yatsunami, T., "Subscale Wind Tunnels and Supplemental Studies of Scramjet Engine Tests," Technical Report of National Aerospace Laboratory, TR-1458(in Japanese), 2003.