Basic characteristics of the free-piston driven expansion tube JAXA HEK-X
Author:
Affiliation:
1. Japan Aerospace Exploration Agency (JAXA)
2. Tokai University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-3817
Reference6 articles.
1. Morgan, R.G., McIntyre, T.J., Buttsworth, D.R., Jacobs, P.A., Potter, D.F., Brandis, A.M., Gollan, R.J., Jacobs, C.M., Capra, B.R., McGilvray, M. and Eichmann, T. "Impulse facilities for the simulation of hypersonic radiating flow", AIAA Paper No. 2008-4270.
2. MacLean, M., Dufrene, A., Wadhams, T. and Holden, M. "Numerical and experimental characterization of high enthalpy flow in an expansion tunnel facility", AIAA Paper No. 2010-1562.
3. Dufrene, A. and Holden M. "Experimental characterization of the LENS expansion tunnel facility including blunt body surface heating", AIAA Paper No. 2011-0626.
4. Nagata, Y., Wasai, K., Makino, H., Yamada, K., and Abe, T. "Test flow conditions for the expansion tube experiment", AIAA Paper No. 2010-4786.
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