@inproceedings{oai:jaxa.repo.nii.ac.jp:00004257,
 author = {埴田, 亮 and 野村, 聡幸 and 村山, 光宏 and 山本, 一臣 and 金崎, 雅博 and Hanida, Ryo and Nomura, Toshiyuki and Murayama, Mitsuhiro and Yamamoto, Kazuomi and Kanazaki, Masahiro},
 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, In this study, the aerodynamic design of an airfoil for a small blended-wing-body aircraft called novel-wing-body　(NWB) is　discussed. In our previous study, the three dimensional aerodynamic design of NWB was carried out using a typical supercritical airfoil. However, Shock waves near the leading edge of the outer wing appeared, and the wave drag increased. Therefore, the lift-to-drag ratio stayed small. In order to design an ideal airfoil for NWB, The design exploration by Genetic Algorithm (GA) is carried out in this study. Some types airfoils obtained by this exporation are applied to the 3D NWB geometry, and their acrodynamic characteristics are investigated using a three dimensional Navier-Stokes solver. The results show that one of the airfoil obtained can weaken the shock waves near the leading edge of the outer wing., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0061958017, レポート番号: JAXA-SP-12-010},
 pages = {101--107},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {翼胴融合型旅客機の翼型空力設計及び性能検証},
 volume = {JAXA-SP-12-010},
 year = {2013}
}