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Numerical Simulation of Airplane High Lift Device
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Affiliation:

Zhang Bin,Zhan Hao,Zhu Jun(National Key Laboratory of Science and Technology Aerodynamic Design and Research,Northwestern Polytechnical University,Xi'an 710072,China)

Clc Number:

V211.41

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    Abstract:

    High lift device design is a very important task in aircraft design.In this paper,based on the multi-block grid,two turbulence models(SST Fully turbulent and SST Gamma Theta model) are used for numerical simulation of three-dimensional high lift device to study the characteristic of aerodynamic and flow filed,and the applicability of the different turbulence model is studied by comparing the numerical simulation results with wind tunnel experimental results.

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Zhang Bin, Zhan Hao, Zhu Jun. Numerical Simulation of Airplane High Lift Device[J]. Advances in Aeronautical Science and Engineering,2011,2(1):61-65

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History
  • Received:
  • Revised:
  • Adopted:
  • Online: January 13,2012
  • Published: