@inproceedings{oai:jaxa.repo.nii.ac.jp:00004144,
 author = {小澤, 宇志 and 鈴木, 俊之 and 藤田, 和央 and Ozawa, Takashi and Suzuki, Toshiyuki and Fujita, Kazuhisa},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication},
 month = {Nov},
 note = {5th Symposium on Integrating CFD and Experiments in Aerodynamics (October 3-5, 2012, Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)), Chofu, Tokyo, Japan, The hypersonic rarefied wind tunnel has lately been developed at JAXA. The characteristics of hypersonic rarefied flows have been investigated experimentally and numerically in this work. Using a sphere pendulous model, the test flow has been probed by measuring its displacement due to the aerodynamic force. In addition, a spatial variation of total pressure of the test flow has also been measured by using total pressure tubes. The flow field from a conical nozzle to a test section was simulated by computational fluid dynamics/direct simulation Monte Carlo loosely coupled computations, and the flow fields were deduced by integrating experimental and numerical results. Consequently, a 25-mm hypersonic rarefied core flow was obtained using a 45-degree conical nozzle with a Mach number greater than 10 and a Knudsen number greater than 0.1., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0062070036, レポート番号: JAXA-SP-13-001E},
 pages = {407--415},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {Integration between Measurements and Particle Simulations for Hypersonic Rarefied Flows},
 volume = {JAXA-SP-13-001E},
 year = {2013}
}