Insights into Airframe Aerodynamics and Rotor-on-Wing Interactions from a 0.25-Scale Tiltrotor Wind Tunnel Model

著录项

• 来源
  《AHS International technical specialist meeting on aerodynamics, acoustics, and test and evaluation》|2002年|p.1-14|共14页
• 会议地点 San Francisco CA(US)
• 作者

  L.A. Young; D. Lillie; M. McCluer; G.K. Yamauchi; M.R. Derby;

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• 作者单位

  Army/NASA Rotorcraft Division NASA Ames Research Center Moffett Field, CA 94035;

  Army/NASA Rotorcraft Division NASA Ames Research Center Moffett Field, CA 94035;

  Army/NASA Rotorcraft Division NASA Ames Research Center Moffett Field, CA 94035;

  Army/NASA Rotorcraft Division NASA Ames Research Center Moffett Field, CA 94035;

  Aerospace Computing, Inc. Mountain View, CA;

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• 会议组织
• 原文格式 PDF
• 正文语种 eng
• 中图分类 直升机、旋翼机飞行力学;
• 关键词

  c: Wing reference chord length, 2.0833 ft; C_D: Airframe drag coefficient; C_L: Airframe (including wing) lift coefficient; C_N: Wing section normal force coefficient; C_P: Rotor power coefficient et al;

  机译：c：机翼参考弦长，2.0833英尺;; C_D：机体阻力系数;; C_L：机体（包括机翼）升力系数;; C_N：机翼截面法向力系数;; C_P：转子功率系数等;