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Volumn , Issue , 2011, Pages

Flutter speed estimation for folding wing system

Author keywords

Composite wing; Flutter; Folding wing

Indexed keywords


EID: 84875918289     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (5)

References (4)
  • 1
    • 80054997557 scopus 로고    scopus 로고
    • Continuum aeroelastic model for a folding-wing configuration
    • S. Liska and E. H. Dowell "Continuum Aeroelastic Model for a Folding-Wing Configuration". AIAA, Vol. 47, No. 10, pp 2350-2358, 2009.
    • (2009) AIAA , vol.47 , Issue.10 , pp. 2350-2358
    • Liska, S.1    Dowell, E.H.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.