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Volumn 40, Issue 5, 2002, Pages 813-824

Aeroelastic response of nonlinear wing sections using a functional series technique

Author keywords

[No Author keywords available]

Indexed keywords

DAMPING; DEGREES OF FREEDOM (MECHANICS); FEEDBACK CONTROL; FLUTTER (AERODYNAMICS); INCOMPRESSIBLE FLOW; PERTURBATION TECHNIQUES; STIFFNESS; TRANSFER FUNCTIONS;

EID: 0036572754     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1735     Document Type: Article
Times cited : (58)

References (46)
  • 22
    • 0009232765 scopus 로고
    • A methodology for using nonlinear aerodynamics in aeroservoelasticity analysis and design
    • (1991) AIAA Paper , vol.91 , Issue.1110
    • Silva, W.A.1
  • 23
    • 85006880985 scopus 로고    scopus 로고
    • NASA TM-104087, May 1991
  • 24
    • 0027664172 scopus 로고
    • Application of nonlinear systems theory to transonic unsteady aerodynamic responses
    • (1993) Journal of Aircraft , vol.30 , Issue.5 , pp. 660-668
    • Silva, W.A.1
  • 26
    • 0032690340 scopus 로고    scopus 로고
    • Reduced-order models based on linear and nonlinear aerodynamic impulse response
    • April
    • (1999) AIAA Paper , vol.99 , Issue.1262
    • Silva, W.A.1
  • 27
    • 85006937069 scopus 로고    scopus 로고
    • NASA CP-1999-209136/PT1, 1999
  • 29
  • 41
    • 85006928658 scopus 로고    scopus 로고
    • Society for Experimental Mechanics, Bethel, CT, A90-16955 05-39, pp. 1356-1364


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.