한국전산유체공학회:학술대회논문집
- 2011.05a
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- Pages.447-452
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- 2011
CFD Analysis of Aerodynamic Characteristics of Regional Turboprop Aircraft Propeller
중형 터보프롭 항공기급 프로펠러 공력특성 전산해석
- Choi, W. ;
- Choi, J.S. ;
- Jung, I.M. ;
- Kim, J.H. ;
- Lee, I.W. ;
- Han, S.H. ;
- Won, Y.S.
- 최원 (한국항공우주산업(주) 개발본부 고정익선행연구팀) ;
- 최재승 (한국항공우주산업(주) 개발본부 고정익선행연구팀) ;
- 정인면 (한국항공우주산업(주) 개발본부 고정익선행연구팀) ;
- 김지홍 (한국항공우주산업(주) 개발본부 고정익선행연구팀) ;
- 이일우 (한국항공우주산업(주) 개발본부 고정익선행연구팀) ;
- 한성훈 (델타이에스 연구소) ;
- 원영수 (델타이에스 연구소)
- Published : 2011.05.26
Abstract
Propeller shall have high efficiency and improved aerodynamic characteristics to get the thru5t to fly at high speed for the Regional turboprop aircraft. That is way Clark-Y airfoil which is used to conventional turboprop aircraft propeller is selected as a blade airfoil. Adkins method is used for aerodynamic design and performance analysis with respect to the propeller design point. Adkins method is based on the vortex-blade element theory which design the propeller to satisfy the condition for minimum energy loss. propeller geometry is generated by varying chord length and pitch angle at design point of Regional turboprop aircraft. The propeller design results indicate that is evaluated to be properly constructed, through analysis of propeller aerodynamic characteristics using the Meshless method and MRF, SM method.
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