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http://dx.doi.org/10.6108/KSPE.2015.19.6.081

A Study on the Hypersonic Air-breathing Engine Ground Test Facility Composition and Characteristics  

Lee, Yang-Ji (Engine System Research Team, Korea Aerospace Research Institute)
Kang, Sang-Hun (Aerospace System Engineering Department, Sejong University)
Yang, Soo-Seok (Aero propulsion Division, Korea Aerospace Research Institute)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.19, no.6, 2015 , pp. 81-90 More about this Journal
Abstract
In order to know the characteristics of the hypersonic air-breahting engine, high altitude and Mach number ground test is necessary. Therefore, high pressure and high temperature condition should be simulated to do ground test of the hypersonic air-breathing engine. In this paper, the hypersonic air-breathing engine ground test facility of the Korea Aerospace Research Institute was introduced and the composition and characteristics were described.
Keywords
Hypersonic Air-breathing Engine Ground Test Facility; Hypersonic Air-breathing Propulsion System; Air Ejector System; Pitot-rake; Normal Shock Efficiency;
Citations & Related Records
Times Cited By KSCI : 4  (Citation Analysis)
연도 인용수 순위
1 Lee, Y.J., Kang, S.H. and Yang, S.S., "Development of the Scramjet engine Test Facility in Korea Aerospace Research Institute," 27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Chicago, IL, U.S.A., AIAA 2010-4792, Jun. 2010.
2 Lee, Y.J., Cha, B.J., Yang, S.S. and Kim, H.J., "Preliminary Design of Supersonic Ground Test Facility," Journal of the Korean Society of Propulsion Engineers, Vol. 7, No. 4, pp. 53-62, 2003.
3 Lee, Y.J., Kang, S.H., Park P.M. and Yang, S.S., "Design and Manufacture of the Storage Air Heater for Supersonic Ground Test Facility," AICFM9-167, 2007.
4 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.   DOI
5 Lee, Y.J., Cha, B.J. and Yang, S.S., "A Study On the Ejector Design Technique And Flow Characteristics," Journal of the Korean Society of Propulsion Engineers, Vol. 10, No. 1, pp. 54-63, 2006.
6 Lee, Y.J., Kang, S.H., Yang, S.S. and Kwon, S.J., "Starting Characteristics of the Hypersonic Wind Tunnel with the Mach number Variation," Journal of Mechanical Science and Technology, Vol. 28, No. 6 pp. 15-22, 2014.   DOI
7 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," NAL TR-1458, 2003.
8 Grunnet, J.L. and Laster, M.L., "Pressure Recovery in Hypersonic Engine Test Facilities," Journal of Spacecraft and Rockets, Vol. 4, No. 5, pp. 643-649, 1967.   DOI