한국가시화정보학회지 (Journal of the Korean Society of Visualization)

  • 제8권2호
  • /
  • Pages.23-30
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  • 2010
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  • 1598-8430(pISSN)
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  • 2093-808X(eISSN)
한국가시화정보학회 (The Korean Society of Visualization)
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덕트형상에 따른 동축반전 로터블레이드 주위의 전산유동해석

Computational Flow Analysis around Coaxial Rotor Blades with Various Ducts

  • 김수연 (순천대학교 대학원 우주항공공학과) ;
  • 최종욱 (순천대학교 기계우주항공공학부) ;
  • 김성초 (순천대학교 기계우주항공공학부)
  • 투고 : 2010.04.27
  • 심사 : 2010.06.12
  • 발행 : 2010.06.30
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초록

Regarding the aircrafts with a rotor blade system, the miniaturization of them is limited due to the rotor blade length and the tail rotor system. To miniaturize an aircraft, an equipment is required that increases thrust and also shortens the length of the rotor blade. The present study will conduct the flow analysis for miniaturizing the aircraft by applying a duct to the coaxial rotor blade system without tail rotor. First, the verification on the calculated results was conducted through the computational flow analysis on the coaxial rotor blade system without a duct. Then, the flow analysis for the coaxial rotor blade systems was performed including Ka-60 duct, Single duct, Twin duct, and Double duct, respectively. From the numerical results, the thrust coefficient appeared higher with the duct than without a duct for the coaxial rotor blade system. Especially, in the case of Double duct, the thrust was improved due to the increase of incoming flow and the extension of the wake area. These results will be used as the basic concepts for miniaturizing the aircraft with the rotor blade system. The flow analysis on the coaxial rotor blade system including the fuselage remains as a future work.

키워드

참고문헌

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피인용 문헌

  1. Flow Analysis around Tilt-rotor Aircraft at Various Tilt Angles vol.9, pp.2, 2011, https://doi.org/10.5407/JKSV.2011.9.2.040