@inproceedings{oai:jaxa.repo.nii.ac.jp:00037245,
 author = {新井, 隆景 and 森田, 修至 and 永田, 晴紀 and 杉山, 弘 and Arai, Takakage and Morita, Shuji and Nagata, Harunori and Sugiyama, Hiromu},
 book = {航空宇宙技術研究所特別資料, Special Publication of National Aerospace Laboratory},
 month = {Jan},
 note = {30 Sep.-1 Oct. 1997 (21st). 26-27 Mar. 1998 (22nd), 30 Sep.-1 Oct. 1997 (21st). 26-27 Mar. 1998 (22nd), スクラムジェット燃焼器における混合流れ場を調べるため、後向きステップを有するマッハ1.8冷空気流に垂直に水素を噴射した。定温度のPt線での触媒反応を用いて、H2やO2の濃度を測定した。この触媒反応による放熱量は触媒表面のH2やO2の濃度に相当する。この放熱量を空間的に測定し、H2やO2の局所濃度が明らかになった。その結果、混合層において超音速燃焼に対して良い混合状態になると思われる2つの領域が存在することがわかった。, Hydrogen was injected normally to a Mach 1.8 cold air stream with a backward facing step to investigate mixing flow field in a scramjet combustor. Catalytic reaction on constant temperature Pt wire was used to measure the concentration of H2 and/or O2. The amount of heat release due to the catalytic reaction, which corresponds to the concentration of H2 and/or O2 on the surface of the catalyst, was measured spatially so that the local H2 and/or O2 concentration was cleared. The results showed that there were two core regions, which would have good mixing condition for supersonic combustion, in the mixing layer., 資料番号: AA0001655022, レポート番号: NAL SP-40},
 pages = {83--86},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {定温白金線の触媒反応を用いた超音速乱流混合の評価},
 volume = {40},
 year = {1999}
}