@inproceedings{oai:jaxa.repo.nii.ac.jp:00006586,
 author = {神田, 淳 and 甲斐, 高志 and 水藤, 貴靖 and 中道, 二郎 and Kanda, Atsushi and Kai, Takashi and Suito, Takanobu and Nakamichi, Jiro},
 book = {宇宙航空研究開発機構特別資料: 第67回　風洞研究会議論文集, JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 67th Meeting},
 month = {Mar},
 note = {NAL (National Aerospace Laboratory of Japan) cooperates with NASDA (National Space Development Agency of Japan) to verify the design of the H-2A Auxiliary Engine Support Structures that are located between SSBs of the H-2A launch vehicle No.2. It is very difficult to know beforehand fluctuating aerodynamic loads applied to actual support structures. This paper shows how to verify the design of support structures. Moreover, results of wind tunnel tests in NAL Transonic Wind Tunnel (TWT-1) are shown., 資料番号: AA0047429002, レポート番号: JAXA-SP-03-004},
 pages = {9--13},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {H-2A補助エンジントラス設計検証と遷音速風洞実験},
 volume = {JAXA-SP-03-004},
 year = {2004}
}