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Volumn 16, Issue 11-12, 2005, Pages 1051-1056

Aeroelastic considerations on shape control of an adaptive wing

Author keywords

Adaptive camber; Aeroelasticity; Morphing wing; Shape control

Indexed keywords

ACTUATORS; ALGORITHMS; COMPUTER SIMULATION; DEFORMATION; FEEDBACK CONTROL; NUMERICAL ANALYSIS; PIEZOELECTRIC DEVICES; WINGS;

EID: 27844461487     PISSN: 1045389X     EISSN: None     Source Type: Journal    
DOI: 10.1177/1045389X05059965     Document Type: Conference Paper
Times cited : (34)

References (13)
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  • 2
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  • 3
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    • Aerodynamic and aeroelastic characteristics of a variable-span morphing wing
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    • Bae, J.S.1    Seigler, T.M.2    Inman, D.J.3
  • 4
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    • Evaluating the impact of morphing technologies on aircraft performance
    • April
    • Bowman, J., Sanders, B. and Weisshaar, T. April 2002. "Evaluating the Impact of Morphing Technologies on Aircraft Performance," AIAA Paper 2002-1631.
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  • 5
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  • 8
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    • A model to compare the flight control energy requirements of morphing and conventionally actuated wings
    • April
    • Johnston, C.O., Neal, D.A., Wiggins, L.D., Robertshaw, H.H., Mason, W.H. and Inman, D.J. April 2003. "A Model to Compare the Flight Control Energy Requirements of Morphing and Conventionally Actuated Wings," AIAA Paper 2003-1716.
    • (2003) AIAA Paper , vol.2003 , Issue.1716
    • Johnston, C.O.1    Neal, D.A.2    Wiggins, L.D.3    Robertshaw, H.H.4    Mason, W.H.5    Inman, D.J.6
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    • A finite-element model for piezoelectric composite laminates
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    • Aerodynamic and aeroelastic characteristics of wings with conformal control surfaces for morphing aircraft
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.