Author:
Kurita Mitsuru,Okada Takumi,Nakamura Yoshiaki
Publisher
Japan Society for Aeronautical and Space Sciences
Reference9 articles.
1. 1) Kavandi, J., Callis, J., Gouterman, M., Khalil, G., Wright, D., Green, E., Burns, D. and McLachlan, B.: Luminescent Barometry in Wind Tunnels, Rev. Sci. Instrum., 61 (1990), pp. 3340–3347.
2. 2) Borovoy, V., Bykov, A., Mosharov, V., Orlov, A., Radchenko, V. and Phonov, S.: Pressure Sensitive Paint Application in Shock Wind Tunnel, 16th ICIASF Record, 1995, 34.1–34.4.
3. 4) Nakakita, K., Yamazaki, T. and Asai, K.: Pressure Sensitive Paint Measurement in a Hypersonic Shock Tunnel, AIAA Paper 2000-2523, 2000.
4. 5) Sakaue, H. and Sullivan, J. P.: Fast Response Time Characteristics of Anodized Aluminum Pressure Sensitive Paint, AIAA Paper 2000-0506, 2000.
Cited by
4 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献