@techreport{oai:jaxa.repo.nii.ac.jp:00045025,
 author = {新野, 正之 and 熊川, 彰長 and 八柳, 信之 and 五味, 広美 and 鈴木, 昭夫 and 坂本, 博 and 佐々木, 正樹 and 柳川, 孝二 and NIINO, Masayuki and KUMAKAWA, Akinaga and YATSUYANAGI, Nobuyuki and GOMI, Hiromi and SUZUKI, Akio and SAKAMOTO, Hiroshi and SASAKI, Masaki and YANAGAWA, Koji},
 month = {Jul},
 note = {This is the final report on “A Study of Liquid Hydrogen Cooled LO2/LH2 Rocket Combustor”which has been conducted as a NAL-NASDA joint research program since 1977. Heretofore, an experimental investigation was conducted to determine the cooling characteristics of LH2 and combustion efficiency characteristics by using a sub-sized combustor with channel wall construction. In this report thermo-hydraulic behavior of the coolant in the channels of the combustor was investigated by using an improved combustor. The following conclusions are based on studies of two combustors. 1)Liquid hydrogen heat transfer correlations including the asymmetric heating effects were derived. These empirical equtions were able to predict over 95％ of all the present experimental data within ±20％ errors. 2)The correlation for the characteristic velocity efficiency was empirically derived. The equation succeeded in correlating all data within ±2％ errors. To verify the usefulness of these results, the relationships between the present subsized combustors and the full-sized“LE-5”engine, were discussed., 資料番号: NALTR0767000, レポート番号: NAL TR-767},
 title = {小型溝構造液水冷却燃焼器の研究(第3報)(大型燃焼器との関連性)},
 year = {1983}
}