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Volumn 21, Issue 2, 2008, Pages 187-192

Optimal design of compliant trailing edge for shape-changing

Author keywords

Adaptive wing; Compliant mechanism; Distributed pressure load; Genetic algorithm; Geometric nonlinearity; Topology optimization

Indexed keywords

ADAPTIVE SYSTEMS; GENETIC ALGORITHMS; MATLAB; PRESSURE DISTRIBUTION; SHAPE OPTIMIZATION;

EID: 42949132297     PISSN: 10009361     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1000-9361(08)60024-2     Document Type: Article
Times cited : (49)

References (14)
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    • A Musolff QD Mao YY Liu Adaptive airfoil with shape memory alloys Journal of Engineering Design 10 1 2003 26 31 [in Chinese].
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    • L Saggere S Kota Static shape control of smart structures using compliant mechanisms AIAA Journal 37 5 1999 572 578
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    • Lu K J. Synthesis of shape morphing compliant mechanisms. PhD thesis, University of Michigan, 2004.
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    • Good M G. Development of a variable camber compliant aircraft tailing using structure optimization. Master thesis, Virginia Polytechnic Institute and State University, 2004.
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    • Kota S, Hetrick J A. Adaptive compliant wing and rotor system. U.S. Patent No 60/451, 812, 2003.
  • 8
    • 85120124616 scopus 로고    scopus 로고
    • Synthesis of flexible mechanisms for airfoil shape control: a modal procedure
    • LF Campanile Synthesis of flexible mechanisms for airfoil shape control: a modal procedure German Aerospace Center (DLR) 2004
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    • Campanile, LF1
  • 9
    • 85120094094 scopus 로고    scopus 로고
    • Buhl T. Compliant mechanism design for adaptive trailing edge flaps. XXI International Congress of Theoretical and Applied Mechanics Warsaw. 2004.
  • 10
    • 85120139659 scopus 로고    scopus 로고
    • Air force validate and flight-test compliant trailing edge. (2006-12-26) [2007-01-11]
    • Y Zhang Air force validate and flight-test compliant trailing edge. (2006-12-26) [2007-01-11] http://jczs.news.sina.com.cn/p/2006-12-26/1358422474.html
    • Zhang, Y1
  • 12
    • 35348961448 scopus 로고    scopus 로고
    • Investigation on synthesis optimization for shape morphing compliant mechanisms using GA
    • X Chen WJ Ge YH Zhang Investigation on synthesis optimization for shape morphing compliant mechanisms using GA Acta Aeronautica et Astronautica Sinica 28 5 2007 1230 1235 [in Chinese].
    • (2007) Acta Aeronautica et Astronautica Sinica , vol.28 , Issue.5 , pp. 1230-1235
    • Chen, X1    Ge, WJ2    Zhang, YH3
  • 13
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    • Topology optimization of the compliant mechanism for shape change of airfoil leading edge
    • J Huang WJ Ge F Yang Topology optimization of the compliant mechanism for shape change of airfoil leading edge Acta Aeronautica et Astronautica Sinica 28 4 2007 988 992 [in Chinese].
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.