@inproceedings{oai:jaxa.repo.nii.ac.jp:00036740,
 author = {矢嶋, 良夫 and 佐野, 理 and Yajima, Yoshio and Sano, Osamu},
 book = {航空宇宙技術研究所特別資料, Special Publication of National Aerospace Laboratory},
 month = {Sep},
 note = {航空宇宙技術研究所 Sep. 1994 (15th). Mar. 1995 (16th) 東京 日本, National Aerospace Laboratory Sep. 1994 (15th). Mar. 1995 (16th) Tokyo Japan, 水流中の円柱体の周りの速度場および円柱体上の抵抗力の測定を、それぞれレーザ・ドプラー速度計と歪みゲージを用いて行った。円柱やいろいろなタイプの表面粗さを持った翼および1列と2列の孔列を持った翼について試験した。特に、その直径を横切っている2列の孔列のある柱体では、かなりの幅の迎角範囲での抵抗減少が見られた。レイノルズ数が5000-9000の場合の、平滑面を持つ柱体に比べて、38%もの低下となった。, Measurements of the velocity field around and the drag force on cylindrical bodies in water flows were made by means of a laser Doppler velocimeter and strain gauges, respectively. A circular cylinder and an airfoil with different types of surface roughness as well as those with single or double rows of holes were tested. In particular a cylinder with double rows of holes placed across its diameter shows a drag reduction for fairly wide range of attack angle. It amounts to as much as 38 percent in comparison to a smooth surfaced cylinder in the Reynolds number range of 5,000-9,000., 資料番号: AA0000109011, レポート番号: NAL SP-28},
 pages = {45--49},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {孔列のある2次元物体を過ぎる流れと抵抗},
 volume = {28},
 year = {1995}
}