@inproceedings{oai:jaxa.repo.nii.ac.jp:00004908,
 author = {鈴木, 俊之 and 大澤, 弘始 and 高柳, 大樹 and 水野, 雅仁 and 藤田, 和央 and 澤田, 恵介 and Suzuki, Toshiyuki and Osawa, Hiroshi and Takayanagi, Hiroki and Mizuno, Masahito and Fujita, Kazuhisa and Sawada, Keisuke},
 book = {宇宙航空研究開発機構特別資料: 第41回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2009論文集, JAXA Special Publication: Proceedings fo 41st Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2009},
 month = {Feb},
 note = {平成21年6月18-19日. 宇宙航空研究開発機構調布航空宇宙センター, 18 June-19 June, 2009, Japan Aerospace Exploration Agency, Direct simulation Monte Carlo code is developed to study a catalytic process of atomic oxygen on thermal protection material surface. The present method employs the phenomenological electronic excitation model and the heterogeneous catalytic model. Numerical method is applied to simulate the flowfield around a test piece put into the rarefied dissociating oxygen test flow. The calculated number density ratio of oxygen to argon is compared with the measured emission intensity ratio of oxygen line to argon line. The sensitivity analysis is made by varying Eley-Rideal reaction cross section under the several conditions of collisional desorption cross section, sticking coefficient, and total number of surface site. It is found from the study that the probability value of Eley-Rideal reaction for the test piece made of a sintered silicon carbide is about 0.035, while the value of about 0.1 is deduced for the test piece made of copper., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064672010, レポート番号: JAXA-SP-09-011},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {触媒性再結合反応モデル構築に向けた触媒性計測装置内部希薄流れ場の数値解析},
 volume = {JAXA-SP-09-011},
 year = {2010}
}