@article{oai:jaxa.repo.nii.ac.jp:00032097,
 author = {浅沼, 強 and 高久, 有幹 and 岡島, 厚 and 谷勝, 達哉 and ASANUMA, Tsuyoshi and TAKAKU, Aritomo and OKAJIMA, Atsushi and TANIKATSU, Tatsuya},
 issue = {2_A},
 journal = {東京大学宇宙航空研究所報告},
 month = {Apr},
 note = {一様流れの中で並進振動する楕円翼(翼厚比20%)の動特性を調べる目的から,新しく開発した12個の貼付式示圧計を翼面上に装着して振動翼面上の局所的な圧力分布を測定した.その際,レイノルズ数,迎え角および強制振動数を広い範囲に変えながら翼に働く法線力も同時に測定した.その結果,無失速もしくは失速状態における翼面上の圧力分布に著しい相違のあることが明らかになった.なお,これら圧力分布から求めた法線力を直接測定した法線力と比較したところ,両者はよく一致していることがわかった., In order to analyze the dynamic characteristics of an elliptic airfoil oscillating in uniform flow, the distributions of steady and unsteady pressure over the surface of the airfoil are measured simultaneously by using many newly developed miniature pressure transducers. These transducers were especially designed to be easily and directly applied to any arbitrary spot on the moving surface. Measurements are carried out while changing Reynolds number, angle of attack, and frequency of airfoil oscillation. Analysis of these measurements indicates that the characteristics of the pressure distribution depend essentially on whether or not the airfoil is operating in the stalled state. Furthemore, the normal forces calculated from the pressure distributions are found to be in good agreement with those measured directly by means of a strain gauge., 資料番号: SA0125204000},
 pages = {323--341},
 title = {並進振動する楕円翼面上の変動圧力の測定},
 volume = {9},
 year = {1973}
}