TIME-ACCURATE FREE-VORTEX WAKE MODEL FOR DYNAMIC ROTOR RESPONSE

著录项

• 来源
  《American Helicopter Society aeromechanics specialists meeting (Aeromechanics 2000)》|2000年|p.1-19|共19页
• 会议地点 Atlanta GA(US);Atlanta GA(US)
• 作者

  Mahendra J. Bhagwa; J. Gordon Leishman;

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• 作者单位

  Alfred Gessow Rotorcraft Center,Department of Aerospace Engineering, Glenn L. Martin Institute of Technology,University of Maryland, College Park, Maryland 20742 mrb@eng.umd.edu;

  Alfred Gessow Rotorcraft Center,Department of Aerospace Engineering, Glenn L. Martin Institute of Technology,University of Maryland, College Park, Maryland 20742 leishman@eng.umd.ed;

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• 会议组织
• 原文格式 PDF
• 正文语种 eng
• 中图分类 基础理论及试验;
• 关键词

  a: speed of sound; cn: blade section normal force coefficient,rnN/(1/2rU~2c); cref: blade reference chord; CP: rotor power coefficient, P/r(WR)3A =rnQ/r(WR)2RA; CT: rotor thrust coefficient, T/r(WR)2A (shaft axes);

  机译：a：声速;; cn：叶片截面法向力系数，rnN /（1 / 2rU〜2c）;; cref：叶片基准弦;; CP：转子功率系数，P / r（WR）3A = rnQ / r （WR）2RA ;; CT：转子推力系数，T / r（WR）2A（轴轴）;