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基于涡量场的二维物体气动力计算

Calculation of the Unsteady Aerodynamics Based on Two Dimensional Vorticity Field
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摘要 提出了在有限流场区域中根据涡量场计算二维物体气动力的两个公式。在FLUENT数值模拟得到的流场中,运用提出的两个公式,计算了雷诺数为1000的二维无厚度平板的气动力。按照不同方法计算得到的结果接近。提出的两个公式比Noca的FLUX和MOMENTUM公式在形式上简单,便于使用。 Two formulas to calculate the force of the object in the limited flow field according to vorticity field were proposed. In the flow field numerically simulated by FLUENT, the forces of a fiat plate with Re number 1000 was calculated by the two formulas. The results from different methods are close. The proposed two formulas are simpler than Noca's FLUX and MOMENTUM equations.
作者 马明 程用胜
出处 《微型电脑应用》 2013年第4期47-49,共3页 Microcomputer Applications
关键词 气动力 涡量场 涡量矩定理 Aerodynamic Force Vorticity Field Vorticity Moment Theorem
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参考文献4

  • 1Noca F, Shiels D, Jeon D A comparison of methods for evaluating time-dependent fluid dynamic forces on bodies, using only velocity fields and their derivatives[J]. Journal of Fluids and Structures, 1999, 13(5): 551-578.
  • 2Jardin T, Chatellier L, Farcy A, David L. Correlation between vortex structures and unsteady loads for flapping motion in hover. Experiments in Fluids, 2009, 47(4-5): 655-664.
  • 3Ferreira C, Bussel G, Scarano F, Kuik G. PIV Visualiza- tion of Dynamic Stall VAWT and Blade Load Determi- Exhibit [C].46th AIAA Aerospace Sciences Meeting al~d 2008, Reno, Nevada.
  • 4Wu J C. Elements of Vorticity Aerodynamics[M]. Bei- jing: TsinghuaUniversity Press: 2005.

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