二次元翼の非定常力に与える非線形因子の影響

書誌事項

タイトル別名
  • The effects of nonlinearity on the unsteady force of two-dimensional airfoils.
  • 2ジゲンヨク ノ ヒテイジョウリョク ニ アタエル ヒセンケイ インシ ノ エ

この論文をさがす

抄録

The effects of nonlinearity on unsteady force in two-dimensional potential flow are studied. The nonlinearities of airfoil thickness, camber and angle of attack have the effect to retarding the build-up of lift, whereas the wake-deformation has an opposite effect. The thickness and camber also have the effect of increasing the force of apparent mass which is proportional to the acceleration of the flow. The general formula to obtain the initial lift and drag of impulsively started airfoils of arbitrary-shape is derived and in the case of Joukowski airfoils, the solution is compared with Chow and Huang's approximate solution, which is valid when the camber is slight and angle of attack is small.

収録刊行物

被引用文献 (1)*注記

もっと見る

キーワード

詳細情報 詳細情報について

問題の指摘

ページトップへ