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对称双翼沉浮振动推进性能研究 被引量:2

Performance investigation of symmetrical plunging dual-foils propulsor
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摘要 该文利用非定常双时间NS方程的预处理方法对摆翼地效推进器进行了推力和推进性能的分析,结果显示沉浮振动的推力和效率与速度的变化关系表现出一致性;固定频率,改变速度,发现推力和效率存在极大值点;随着频率增大,极大值点右移。最大推力和效率的动力攻角为6o-9o,利用速度矢量图和压力云图显示了分离涡的输运和扩散,再一次展示了地效的存在。 The preconditioning method for unsteady dual-time NS equations is employed to evaluate and analyze the performance of symmetrical plunging dual-foils. The calculated result shows that the trend of relations between efficiency and thrust versus speed agreed well with previous experimental measurement. For a fixed frequency and changing speed, the maximum thrust and efficiency may be obtained and with the increment of fixed frequency the points of maximum thrust and efficiency are shifted rightward. The danamic angles of attack corresponding to the points of maximum thrust and efficiency fall in the interval between 6 to 9 degrees. The transporation and diffusion of vortex separation are showed by using the vecdor graph and pressure nephogram and in which the wing-in-ground effect is revealed and resulted in the increment of averageci thrust and efficiency
作者 王涛
出处 《水动力学研究与进展(A辑)》 CSCD 北大核心 2009年第5期647-653,共7页 Chinese Journal of Hydrodynamics
基金 国家自然科学基金项目(40576047)
关键词 NS方程 翼形振动 地效推进技术 NS equations symmetrical plunging dual-foils ground effect propulsion
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  • 1张晓庆,王志东,张振山.二维摆动水翼仿生推进水动力性能研究[J].水动力学研究与进展(A辑),2006,21(5):632-639. 被引量:24
  • 2陆夕云,杨基明,尹协振,童秉纲.飞行和游动的生物运动力学和仿生技术研究[J].中国科学技术大学学报,2007,37(10):1159-1163. 被引量:9
  • 3KNOLLER R. Die Gesetze des luftwiderstandes[J]. Flug und Motortechnik (Wien) , 1909, 3(21) :1-7.
  • 4BETZ A. Ein beitrag zur erklaerung des segelfluges[J]. Zeitschrift fuer Flugtechnik und Motorluftschiffahrt, 1912, 3: 269-272.
  • 5KATZMAYR R. Effect of periodic changes of angle of attack on behavior of airfoils[R]. NACA Report. Oct,1922.
  • 6Von KARMAN T, BURGERS J M. General aerodynamic theo- ry-perfect fluids[M]. Division E, Vol. II, Aerodynamic Theo- ry, Ed. Durand, W. F. , 1943. 308.
  • 7GARRICK I E. Propulsion of a flapping and oscillating airfoil [R]. NACA Technical Report, JONES K D, PLATZER M F. 1936, (567).
  • 8Numerical computation of flap- ping-wing propulsion and power extraction[R]. AIAA 97-0826, 1997.
  • 9杨亮.仿金枪鱼摆动尾鳍的水动力性能与推进机理研究[D].哈尔滨:哈尔滨工程大学,2009.
  • 10YANG S, LUO S, LIU F. Computation of the flows over flap- ping airfoil by the euler equations[A]. The AIAA 43rd Aero- space Sciences Meeting, Reno[C]. NV, 10-13, 2005.

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