Author:
MATSUKAWA Yutaka,DOIGUCHI Kaname
Publisher
Japan Society for Aeronautical and Space Sciences
Reference18 articles.
1. 1) Olejniczak, J., Wright, M., Laurence, S. and Hornung, H.: Computational Modeling of T5 Laminar and Turbulent Heating Data on Blunt Cones, Part 1: Titan Applications, AIAA Paper 2005-0176, 2005.
2. 2) Tanno, H., Komuro, T., Sato, K., Itoh, K., Yamada, T., Sato, N. and Nakano, E.: Heat Flux Measurement of Apollo Capsule Model in the Free-Piston Shock Tunnel HIEST, AIAA Paper 2009-7304, 2009.
3. 3) Tanno, H., Kodera, M., Komuro, T., Sato, K., Takahashi, M. and Itoh, K.: Aeroheating Measurements on a Reentry Capsule Model in Free-Piston Shock Tunnel HIEST, AIAA Paper 2010-1181, 2010.
4. 4) Matsukawa, Y.: Equilibrium Calculation of Augmented Shock-Tunnel Heat Flux at High-Pressure and High-Enthalpy Conditions, J. Thermophys. Heat Trans., 25 (2011), pp. 632-634.
5. 8) Ishihara, T., Ogino, Y., Sawada, K. and Tanno, H.: Computation of Surface Heat Transfer Rate on Apollo CM Test Model in Free-Piston Shock Tunnel HIEST, AIAA Paper 2012-0285, 2012.