Development of Rotor Blade with Low-Noise and High-Efficiency

저소음 고효율 로터깃 개발에 관한 연구

  • 신성룡 (서울대학교 공력소음 및 소음제어 연구실) ;
  • 선효성 (서울대학교 공력소음 및 소음제어 연구실) ;
  • 이수갑 (서울대학교 기계항공우주공학부) ;
  • 남찬진 (현대우주항공) ;
  • 강인준 (현대우주항공)
  • Published : 2000.06.22

Abstract

Integrated tools are developed for the analysis of the aerodynamic performance and aeroacoustics of helicopter rotors. Heli-NK(Helicopter Navier-Stokes & Kirchhoff) code is for hovering and heli-PA(Helicopter Panel & Acoustic analogy) for forward flight. The former showed its ability to predict the hovering efficiency and high-speed impulsive noise level. Thrust calculation, noise levels, and noise directivity patterns are investigated to confirm the availability of the latter. With some proper validation and improvements. these codes will be more useful and practical.

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