Advanced Hypersonic Test Facilities
This book presents a number of new, innovative approaches to satisfy the enthalpy requirements for air-breathing hypersonic vehicles and planetary entry problems.
TABLE OF CONTENTS Advanced Hypersonic Test Facilities
References
1 Hertzberg, A., Wittliff, C. E., and Hall, J. G., "Summary of Shock Tunnel Development and Application in Hypersonic Research," AFOSR TR 60 139, Cornell Aeronautical Laboratories, 1961.
2 Stalker, R. J., "A Study of the Free-Piston Shock Tunnel," AIAA Journal, Vol. 5, No. 12, 1967, pp. 2160 2165.
3 Bird, G. A., "A Note on Combustion Driven Shock Tubes," AGARD Report No. 146, 1957.
4 Yu, H. R., "Shock Tunnel and its Application to Aeroheating Experiments," [in Chinese], Thesis, Institute of Mechanics, Chinese Academy of Sciences, Beijing, 1963.
5 Yu, H. R., "Recent Developments in Shock Tube Applications," Proceedings of the 1989 Japanese National Symposium on Shock Wave Phenomena, Sagamihara, Japan, 1989, pp. 1 7.
6 Yu, H. R., "Oxyhydrogen Combustion and Detonation Driven Shock Tube," Acta Mechanica Sinica, Vol. 15, No. 2, 1999, pp. 97 107.
7 Yu, H. R., Esser, B., Lenartz, M., and Gr ig, H., "Gaseous Detonation Driver for a Shock Tunnel," Shock Waves, Vol. 2, No. 4, 1992, pp. 245 254.
8 Bakos, R. J., Calleja, J. F., Erdos, J. I., Sussman, M. A., and Wilson, G. J., "An Experimental and Computational Study Leading to New Test Capabilities for the HYPULSE Facility with a Detonation Driver," AIAA Paper 96 2193, 1996.
9 Bakos, R. J., Castrogiovanni, A., Calleja, J. F., Nucci, L., and Erdos, J. I., "Expansion of the Scramjet Ground Test Envelope of the HYPULSE Facility," AIAA Paper 96 4506, 1996.
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