Improved Two-Dimensional Dynamic Stall Prediction with Structured and Hybrid Numerical Methods

著录项

• 来源
  《Journal of the American Helicopter Society》 |2011年第4期|p.042007.1-042007.12|共12页
• 作者

  K. Richter; A. Le Pape; T. Knopp; M. Costes; V. Gleize; A. D. Gardner;

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• 作者单位

  Institute of Aerodynamics and Flow Technology German Aerospace Center (DLR) Gottingen, Germany;

  Applied Aerodynamics Department ONERA Meudon Cedex, France;

  Institute of Aerodynamics and Flow Technology German Aerospace Center (DLR) Gottingen, Germany;

  Applied Aerodynamics Department ONERA Meudon Cedex, France;

  Numerical Simulation and Aeroacoustics Department, ONERA Chdtillon Cedex, France;

  Institute of Aerodynamics and Flow Technology German Aerospace Center (DLR) Gottingen, Germany;

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• 原文格式 PDF
• 正文语种 eng
• 中图分类
• 关键词

  b: span, m; c: chord, m; c_d, Δc_d: drag coefficient, difference in drag coefficient; c_l, ΔC-l: lift coefficient, difference in lift coefficient; c_m, Δc_m: pitching moment coefficient, difference in pitching moment coefficient;

  机译：b：跨度;m;c：和弦;m;c_d;Δc_d：阻力系数;阻力系数之差;c_1;ΔC-1：升力系数;升力系数之差;c_m;Δc_m：俯仰力矩系数;俯仰力矩系数之差;