@inproceedings{oai:jaxa.repo.nii.ac.jp:00003823,
 author = {飯島, 秀俊 and 永井, 伸治 and 西島, 寛典 and 木村, 毅 and Iijima, Hidetoshi and Nagai, Shinji and Nishijima, Hironori and Kimura, Takeshi},
 book = {宇宙航空研究開発機構特別資料: 第86-第90回風洞研究会議論文集, JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 86th-90th meeting},
 month = {Mar},
 note = {第87回風洞研究会議 (2011年11月17日-18日), Wind Tunnel Technology Association 87th Meeting (November 17-18, 2011), Starting loads reduction technique using a protuberance was investigated in the JAXA 1m by 1m supersonic wind tunnel. A protuberance was set upstream from the model on the upper and lower nozzle wall. As a result, it was found that the shock wave by the protuberance induced a decelerated area around the model and reduced more than 20% of the starting load of normal force at a Mach number of 3.0. This deceleration by the shock wave from the protuberance was confirmed by pressure of the model surface. Furthermore, shock wave strength passing through the model was weakened in this decelerated area., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1530024004, レポート番号: JAXA-SP-14-011},
 pages = {21--25},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {突起を用いた起動停止荷重低減法の検討について},
 volume = {JAXA-SP-14-011},
 year = {2015}
}