@inproceedings{oai:jaxa.repo.nii.ac.jp:00005449,
 author = {牧野, 好和 and Makino, Yoshikazu},
 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), JAXA's planned scaled low-boom demonstrator project and its aerodynamic design in conceptual design phase are introduced. For the demonstration of low sonic-boom design concepts and design technology, this demonstrator named Silent SuperSonic Technology Demonstrator (S3TD) is designed using JAXA's computer-based aerodynamic design tools for low-drag and low-boom configuration. A multidisciplinary design exploration, in which the aerodynamic performance estimated by an unstructured Euler CFD code, sonic-boom intensity, and structural constraints are taken into account, is applied to the design of the demonstrator as well as an aerodynamic conceptual design tool based on a low-fidelity panel method. Several design cycles are conducted through the validation process for mission requirement with many CFD analyses and wind-tunnel tests., 形態: カラー図版あり, 資料番号: AA0064239013, 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 = {静粛超音速研究機の空力設計の概要},
 volume = {JAXA-SP-08-008},
 year = {2009}
}