Volume 24 Issue 1
Jan.  1998
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Zhang Jianfeng, Liu Siyong. Application of Semi Rigid Trailing to Ram Air Turbine Performance Calculating[J]. Journal of Beijing University of Aeronautics and Astronautics, 1998, 24(1): 28-30. (in Chinese)
Citation: Zhang Jianfeng, Liu Siyong. Application of Semi Rigid Trailing to Ram Air Turbine Performance Calculating[J]. Journal of Beijing University of Aeronautics and Astronautics, 1998, 24(1): 28-30. (in Chinese)

Application of Semi Rigid Trailing to Ram Air Turbine Performance Calculating

  • Received Date: 10 Jun 1996
  • Publish Date: 31 Jan 1998
  • Rigid trailing vortex model consistent with Goldstein hypothesis is often employed in propelles lifting line (lift surface) calculation on the condition of light load,but presents certain errors on the condition of heavy load.Semi rigid trailing vortex model consistent with Theodorsen hypothesis extents Goldstein trailing vortex to heavy load condition.Application of Theodorsen trailing vortex model to ram air turbine lifting line calculation is discussed.A model ram air turbine has been employed to calculate.The results show reasonable distributions of trailing vortex pitch,induced velocities,circulations and blade element wind power utilization coefficient.Wind power utilization coefficient agrees well with experiments.

     

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  • 1. 张剑锋,刘思永.冲压空气涡轮性能的局部改进的升力线算法,北京航空航天大学学报,1997,22(4):482~486 2. Sullivan J P.The effect of blade sweep on propeller performance.AIAA77 716,1977 3. Theodorsen J.Theory of propellers.New York:McGraw Hill,1948 4. Chiu Y D,Peters D A.Numerical solution of induced veocities by semi infinite tip vortex lines.J Aircr,1988,25(8):684~694
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