한국전산유체공학회:학술대회논문집

Korean Society of Computational Fluids Engineering (한국전산유체공학회)
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THE INVESTIGATION OF THE AERO-ACOUSTIC ANALYSIS METHODS FOR THE HELICOPTER BLADE

헬리콥터 블레이드 공력 소음 해석 기법 연구

  • 박남은 (한국항공우주산업(주)) ;
  • 우철훈 (한국항공우주산업(주)) ;
  • 이상기 (한국항공우주산업(주) KHP로터설계팀) ;
  • 이석준 (한국항공우주산업(주) KHP로터설계팀)
  • Published : 2008.03.26
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Abstract

The development technology for the helicopter is improved by the increasing of computing power and advanced test facilities. The increasing efficiency of fuel consuming by the developing of improved lift-to-drag rotor system is the major issue, the noise reduction for ecology(civil area) and increase of survivability to reduce noise detection(battlefield) also are important. This investigation shows the classification of helicopter external noise and requirements, the noise flight test methods, the numerical modeling method for aero-acoustic of rotor blade and the result of CAA(Computational Aero-Acoustic) for main rotor blade.

Keywords