@techreport{oai:jaxa.repo.nii.ac.jp:00043449,
 author = {海田, 武司 and 荻野, 純 and 高梨, 進 and Kaiden, Takashi and Ogino, Jun and Takanashi, Susumu},
 month = {Nov},
 note = {As various airplanes are increasing recently, aerodynamic design method with high accuracy has been requested about non-planar wings which are tip-fin configuration of HOPE and winglet of civil transport, etc. On non-planar wing design, it is indispensable to using Navier-Stokes code for viscous effect of corner flow and this induced separation It is presented that non-planar wing was designed using inverse method with Navier-Stokes code instead of usual full-potential code. We have applied tip-fin of HOPE to design configuration through the courtesy of NASDA., 資料番号: NALSP0014016, レポート番号: NAL SP-14},
 title = {ナビエ・ストークス逆解法による非平面主翼の空力設計},
 year = {1990}
}