@inproceedings{oai:jaxa.repo.nii.ac.jp:00038777,
 author = {小野寺, 卓郎 and 佐々木, 正樹 and 布目, 佳央 and 森谷, 信一 and 川島, 秀人 and 根岸, 秀世 and 冨田, 健夫 and Onodera, Takuo and Sasaki, Masaki and Nunome, Yoshio and Moriya, Shin'ichi and Kawashima, Hideto and Negishi, Hideyo and Tomita, Takeo},
 book = {第59回宇宙科学技術連合講演会講演集, Proceedings of 59th Space Sciences and Technology Conference},
 month = {Oct},
 note = {第59回宇宙科学技術連合講演会（2015年10月7日-9日. かごしま県民交流センター), 鹿児島市, 鹿児島県, In general, it is very important to rocket engine designs to estimate regenerative cooling performances of rocket engine combustion chambers properly. It was learned from our survey that the data of liquid hydrogen heat transfer characteristics at high pressure was needed to improve the CFD tools for the application to high pressure rocket engine designs. Electrically heated tube tests were conducted in order to get such data. The acquired heat transfer data were compared with the well-known correlations., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AC1600035000, レポート番号: JSASS-2015-4034},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences (JSASS)},
 title = {電気加熱管による高圧液体水素の熱伝達特性取得試験},
 year = {2015}
}