@article{oai:jaxa.repo.nii.ac.jp:00022499,
 author = {徳川, 直子 and 石川, 敬掲 and 戸塚, 絢子 and 上田, 良稲 and Tokugawa, Naoko and Ishikawa, Hiroaki and Tozuka, Ayako and Ueda, Yoshine},
 journal = {Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan},
 month = {},
 note = {In order to design the natural laminar flow nose for the high Reynolds number condition suppressing the increase of pressure drag, “local” and “non-axisymmetric” deformation is applied to a base shape. Through the analysis for low Reynolds number cases, it is confirmed that the localized deformation suppresses the increase of pressure drag, and that non-axisymmetric deformation reduces pressure gradient in the azimuthal direction effectively in order to extend the laminar region. It is also shown that there is a capability of more extension of the natural laminar flow effect to the high Reynolds number condition corresponding to the real civil supersonic transport suppressing the increase of pressure drag., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: PA1420055000},
 pages = {71--80},
 title = {Natural Laminar Flow Nose for Supersonic Transport Designed using Local Non-Axisymmetric Deformation},
 volume = {12},
 year = {2014}
}