@inproceedings{oai:jaxa.repo.nii.ac.jp:00005437,
 author = {坂田, 公夫 and 大貫, 武 and Sakata, Kimio and Ohnuki, Takeshi},
 book = {宇宙航空研究開発機構特別資料: 小型超音速実験機（ロケット実験機）飛行実験データ解析完了報告, JAXA Special Publication},
 month = {Feb},
 note = {小型超音速実験機（ロケット実験機）飛行実験データ解析完了報告会(平成20年7月10日. 東京大学山上会館), National Experimental Supersonic Transport (NEXST) Project was commenced in 1997 and was finalized with the successful flight experiment in 2005. A scaled supersonic aircraft was developed to verify the aerodynamic design technology using Computational Fluid Dynamics (CFD) method. It showed that it would be expected more than 10 % improvement in aerodynamic efficiency compared with the Concord technology., 形態: カラー図版あり, 資料番号: AA0064239001, レポート番号: JAXA-SP-08-008},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {次世代超音速機技術研究開発の概要},
 volume = {JAXA-SP-08-008},
 year = {2009}
}