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주변 구조물을 포함하는 훨타워 로터 블레이드 공력 해석

A NUMERICAL INVESTIGATION OF THE EFFECT OF SURROUNDING BUILDINGS ON THE AERODYNAMIC PERFORMANCE OF A ROTOR SYSTEM ON THE WHIRL TOWER

  • 강희정 (한국항공우주연구원 회전익기술팀)
  • 투고 : 2012.04.18
  • 심사 : 2012.06.01
  • 발행 : 2012.06.30

초록

Numerical calculations were performed to investigate the influence in aerodynamic characteristics of a rotor system by surrounding structures and the ground effect for the rotor blade on a whirl tower is also investigated. Three dimensional Navier-Stokes simulations were carried out by using unstructured overset mesh technique and parallel computation. The calculated hover performance showed good agreement with the experimental result and showed that the structures around the whirl tower did not affect the aerodynamic characteristics of the blade. The ground effect was studied by comparing with the numerical result for the out of ground condition and the result of an analytic model.

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참고문헌

  1. 2007, Jung, M. S, Kang, H. J. and Kwon O. J. "Assessment of Rotor Hover Performance Using a Node-based Flow solver," Int'l J. of Aeronautical and Space Sciences, Vol.8, pp.44-53. https://doi.org/10.5139/IJASS.2007.8.2.044
  2. 1995, V. Venkatakrishnan, "Convergence to Steady State Solutions of Euler Equations on Unstructured Grid with Limiters," Journal of Computational Physics, Vol.118, No.1, pp.120-130. https://doi.org/10.1006/jcph.1995.1084
  3. 2007, Jung, M. S. and Kwon, O. J. "A Parallel Unstructured Hybrid Overset Mesh Technique for Unsteady Viscous Flow Simulations," the International conference on Parallel Computational Fluid Dynamics, ParCFD 2007-024.
  4. 2010, Kim, D. K., Yun, C. Y. and et al., "Performance Test of Helicopter Rotor system in Whirl Tower Test Facility," (in Korean) Proceeding of 2010 KSAS Fall Conference, pp.1422-1425.
  5. 2008, Kang, H. J., Kim, S. H. and et al., "Aerodynamic Calculations in Hover of KUH Rotor Blade," (in Korean) Proceeding of the 5th National Congress on Fluids Engineering, pp.25-28.
  6. 2006, J. Gordon Leishman, Principles of Helicopter Aerodynamics, 2nd edition, Cambridge University Press, pp.258-260.