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Numerical Investigation on Vortex-Structure Interaction Generating Aerodynamic Noises for Rod-Airfoil Models

Author

Listed:
  • FeiFei Liu
  • ShuJie Jiang
  • Gang Chen
  • Yueming Li

Abstract

In past several decades, vortex-structure interaction generated aerodynamic noise became one of the main concerns in aircraft design. In order to understand the mechanism, the acoustic analogy method combined with the RANS-based nonlinear acoustics solver (NLAS) is investigated. The numerical method is firstly evaluated by the experiment data of the classic rod-airfoil model. Compared with the traditional analogy methods, the RANS/NLAS can capture the nonlinear aerodynamic noise more accurately with lower gird requirements. Then different rod-airfoil configurations were simulated to investigate the aeroacoustic interaction effects. The numerical results are in good agreement with those of the earlier experimental research. It is found that the vortex-shedding crash to the airfoil is the main reason for the noise generation which is dependent on the configurations, distance, and flow conditions.

Suggested Citation

  • FeiFei Liu & ShuJie Jiang & Gang Chen & Yueming Li, 2017. "Numerical Investigation on Vortex-Structure Interaction Generating Aerodynamic Noises for Rod-Airfoil Models," Mathematical Problems in Engineering, Hindawi, vol. 2017, pages 1-12, October.
  • Handle: RePEc:hin:jnlmpe:3704324
    DOI: 10.1155/2017/3704324
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