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Volumn 15, Issue 3-4, 2008, Pages 325-334

Optimal design of the active twist for helicopter rotor blades with C-spar

Author keywords

Active twist; C spar; Finite element method; Helicopter rotor blade; Macro fiber composite (MFC); Optimization

Indexed keywords

FINITE ELEMENT METHOD; MATHEMATICAL MODELS; OPTIMIZATION; ROTORS; STATIC ANALYSIS;

EID: 42149137329     PISSN: 15376494     EISSN: 15376532     Source Type: Journal    
DOI: 10.1080/15376490801907855     Document Type: Conference Paper
Times cited : (23)

References (15)
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  • 3
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    • Riemenschneider, J., Keye, S., Wierach P., des and Rochettes, H. M., Overview of the Common DLD/ONERA Project Active Twist Blade (ATB), Proc. 30th European Rotorcraft Forum, 22.1-22.9 (2004).
    • Riemenschneider, J., Keye, S., Wierach P., des and Rochettes, H. M., Overview of the Common DLD/ONERA Project "Active Twist Blade" (ATB), Proc. 30th European Rotorcraft Forum, 22.1-22.9 (2004).
  • 4
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    • Analysis of an actively twisted rotor by multibody global modelling
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    • Ghiringhelli, G.L.1    Masarati, P.2    Mantegazza, P.3
  • 5
    • 0035283855 scopus 로고    scopus 로고
    • On the modelling of integrally actuated helicopter blades
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    • (2001) Int. J. Solids and Structures , vol.38 , pp. 1765-1789
    • Cesnik, C.E.S.1    Shin, S.2
  • 9
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    • Active-Materials induced-strain actuation for aeroelastic vibration control
    • Giurgiutiu, V., "Active-Materials induced-strain actuation for aeroelastic vibration control," The Shock and Vibration Digest, 32(5), pp. 355-368 (2000).
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    • Giurgiutiu, V.1
  • 10
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    • Masarati, P., Morandini, M., and Riemenschneider, J., Wierach, P., Gluhih, S., Barkanov, E., Optimal design of an active twist 1:2.5 scale rotor blade, Proc. 31st European Rotorcraft Forum, 37.1-37.14 (2005).
    • Masarati, P., Morandini, M., and Riemenschneider, J., Wierach, P., Gluhih, S., Barkanov, E., "Optimal design of an active twist 1:2.5 scale rotor blade," Proc. 31st European Rotorcraft Forum, 37.1-37.14 (2005).
  • 12
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    • Auzins, J., Direct optimisation of experimental designs, Proc. 10th AIAA/ISSMO Multidisciplinary Analysis and Optimisation Conf., pp. AIAA 2004-4578 (2004).
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  • 13
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    • Technical Notes No. 562, National Advisory Committee for Aeronautics, Washington, April
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  • 14
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.