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http://dx.doi.org/10.5293/kfma.2012.15.3.019

Aerodynamic Design and Analysis on 1600kW Class Propeller Blade  

Choi, Won (한국항공우주산업(주))
Kim, Kwang-Hae (한국항공우주산업(주))
Won, Young-Su (델타이에스 연구소)
Lee, Won-Joong (한국항공우주연구원 항공안전기술개발사업단)
Publication Information
The KSFM Journal of Fluid Machinery / v.15, no.3, 2012 , pp. 19-24 More about this Journal
Abstract
Propeller shall have high efficiency and improved aerodynamic characteristics to get the thrust to fly at high speed for the turboprop aircraft. That is way Clark-Y airfoil which is used to conventional 1600kW class 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 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.
Keywords
Propeller; Computational Fluid Dynamics; Meshless Method; Multiple Reference Frame; Sliding Mesh;
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  • Reference
1 Colman Shattuck, Jon Young., 1993, "Modern Propeller Technology for Advanced Turboprop Aircraft," AIAA/ SAE/ASME/ASEE 20th Joint Propulsion Conference and Exhibit.
2 R. M. Bass and D. G. M. Davis, 1985, "A Review of Some Recent U.K. Propeller Developments," AIAA/ SAE/ASME/ASEE 21st Joint Propulsion Conference.
3 Lee, K. H, Jeon, Y. H, Bae, E. S, Lee, D. H, Lee, K. T, 2004, "Implementation of the Numerical Optimization for the Micro-Air Vehicle Propeller," 10th AIAA/ ISSMO Multidisciplinary Analysis and Optimization Conference, Albany, New York.
4 Adkins, Charles N., Liebeck, Robert H, 1983, "Design of Optimum Propellers," American Institute of Aeronautices and Astronautics.
5 2011, XFLOW Basic Training Manual.
6 원영수, 민동호, 한성훈, 정영배, 2010. 5, "Meshless CFD SW, XFLOW를 사용한 클린 룸 제조설비 내 기류분석 연구," 한국풍공학회 학술발표회 논문집, pp. 258-263.
7 Phoolan Prasad, 2007, "P. L. Bhatnagar and the BGK Model," 72nd Annual Conference of the Indian Mathematical Society.
8 Next Limit Technologies & qpunkt GmbH, 2010, "Aerodynamic analysis involving moving parts with XFlow".
9 J. A. Lieser, D. Lohmann, C.-H. Rohardt, 1997, "Aeroacoustic Design of a 6-Bladed Propeller," Aerospace Science and Technology, No. 7, pp. 381-389.
10 최원, 김지홍, 이경태, 박찬우, 2010. 5, "MRF 기법을 이용 한 초소형 비행체 프로펠러 공력특성 연구," 한국전산유체공학회, 2010년도 춘계학술발표회 논문집, pp. 94-100.