@inproceedings{oai:jaxa.repo.nii.ac.jp:00004254,
 author = {吉田, 憲司 and Yoshida, Kenji},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication: Proceedings of 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012},
 month = {Mar},
 note = {第44回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2012 (2012年7月5日-6日. 富山国際会議場大手町フォーラム), 富山市, 富山県, 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012 (July 5-6, 2012. Toyama International Conference Center), Toyama Japan, This is a review of aerodynamic research activities on a next generation SST, including some JAXA’s SST research programs (NEXST project, S3 program, D-SEND project). JAXA also proposes a direction of aerodynamic research for realizing a future next generation SST. And JAXA hopes the objectives, plans and goals for those SST researches should be well discussed and shared in Japan near future., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0061958014, レポート番号: JAXA-SP-12-010},
 pages = {79--88},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {次世代超音速旅客機の空力技術に関する研究動向},
 volume = {JAXA-SP-12-010},
 year = {2013}
}