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Volumn 2010, Issue , 2010, Pages

Control of limit cycle oscillations of a two-dimensional aeroelastic system

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTIC SYSTEM; CONTROL OF LIMIT CYCLE; FLUTTER ONSET; FREE-STREAM VELOCITY; LIMIT CYCLE OSCILLATIONS; LINEAR CONTROLS; NON LINEAR CONTROL; NON-LINEAR AERODYNAMICS; NONLINEAR AEROELASTIC SYSTEM; NONLINEAR SPRINGS; NONLINEAR STATICS; NORMAL FORM; SUBCRITICAL HOPF BIFURCATION; SUPER-CRITICAL;

EID: 79953292471     PISSN: 1024123X     EISSN: 15635147     Source Type: Journal    
DOI: 10.1155/2010/782457     Document Type: Article
Times cited : (16)

References (12)
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    • Liu, L.1    Wong, Y.S.2    Lee, B.H.K.3
  • 4
    • 0037284776 scopus 로고    scopus 로고
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  • 7
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    • Abed, E.H.1    Fu, J.-H.2
  • 8
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  • 10
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    • Active aeroelastic control of 2-D wing-flap systems operating in an incompressible flowfield and impacted by a blast pulse
    • DOI 10.1016/j.jsv.2004.05.010, PII S0022460X04004924
    • Librescu L., Na S., Marzocca P., Chung C., Kwak M. K., Active aeroelastic control of 2-D wing-flap systems operating in an incompressible flowfield and impacted by a blast pulse Journal of Sound and Vibration 2005 283 35 685 706 (Pubitemid 40430563)
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    • Bifurcation control via state feedback for systems with a single uncontrollable mode
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.