@article{oai:jaxa.repo.nii.ac.jp:00032287,
 author = {岡島, 厚 and 浅沼, 強 and 高田, 浩之 and OKAJIMA, Atsushi and ASANUMA, Tsuyoshi and TAKATA, Hiroyuki},
 issue = {1_A},
 journal = {東京大学宇宙航空研究所報告},
 month = {Jan},
 note = {一様粘性流れの中で静止および並進振動する楕円肩(肩摩比20%)に働く法線力,モーメントおよび肩面上の圧力分布をレイノルズ数,迎え角そして振動数をそれぞれ広範囲に変えて測定した.それらの測定値を前報の数値解析による計算結果と比較してよく一致することを確認しまた肩が無失速および失速状態で振動する場合について,レイノルズ数,迎え角,振動数の指物を明らかにした.さらにそれらの実測値と平板やミーゼス肩型などに対する非粘性振勃興理論値,定常法線力傾斜や境界層の時間遅れを考慮した修正理論による値および準定常の計算値などと比較検討した., The unsteady normal force, moment and surface pressure exerted on an oscillating elliptic aerofoil of the 20% thickness ratio are measured for the wide ranges of Reynolds number (Re = 40～2 X 10^4), angle of attack (α = 0°～25°) and reduced frequency (k = 0.1～1.4). A good agreement is found between the results of the present experiment and those of the numerical calculation given in the previous paper. From the viewpoint of the viscous effects of flow, influences of Reynolds number, angle of attack and reduced frequency on these aerodynamic forces are discussed for the aerofoil which is in either non-stalled or stalled state. Experimental results are also compared with those of the potential flutter theory for a flat plate or a von Mises profile, those of the modified potential flutter theory proposed by Rott and George, and those predicted by the quasi-steady theory., 資料番号: SA0125461000},
 pages = {1--35},
 title = {並進振動する楕円翼まわりの非定常粘性流れ(その2実験)},
 volume = {8},
 year = {1972}
}