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Volumn 47, Issue 10, 2009, Pages 2350-2358

Continuum aeroelastic model for a folding-wing configuration

Author keywords

[No Author keywords available]

Indexed keywords


EID: 80054997557     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.40475     Document Type: Article
Times cited : (32)

References (16)
  • 2
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    • Morphing UAVs Change the Shape of Warfare
    • Wilson, J. R., “Morphing UAVs Change the Shape of Warfare,” Aerospace America, Vol. 42, No. 2, 2004, pp. 28–29.
    • (2004) Aerospace America , vol.42 , Issue.2 , pp. 28-29
    • Wilson, J.R.1
  • 3
    • 85008303300 scopus 로고    scopus 로고
    • 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Austin, TX, AIAA
    • Lee, D. H., and Weisshaar, T. A., “Aeroelastic Studies on a Folding Wing Configuration,” 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Austin, TX, AIAA, 1998.
    • (1998) Aeroelastic Studies on a Folding Wing Configuration
    • Lee, D.H.1    Weisshaar, T.A.2
  • 4
    • 0034997633 scopus 로고    scopus 로고
    • 42nd Structures, Structural Dynamics, and Material Conference, Seattle, WA, AIAA Paper 2001- 1371, April
    • Radclie, T. O., and Cesnik, C. E. S., “Aeroelastic Response of Multi-Segmented Hinged Wings,” 42nd Structures, Structural Dynamics, and Material Conference, Seattle, WA, AIAA Paper 2001- 1371, April 2001.
    • (2001) Aeroelastic Response of Multi-Segmented Hinged Wings
    • Radclie, T.O.1    Cesnik, C.2
  • 5
    • 85008297945 scopus 로고    scopus 로고
    • CEAS International Forum on Aeroelasticity and Structural Dynamics, Madrid, 5–7 June
    • Radcliffe, T. O., and Cesnik, C. E. S., “Aeroelastic Behavior of Multi-Hinged Wings,” CEAS International Forum on Aeroelasticity and Structural Dynamics, Madrid, 5–7 June 2001, pp. 449–459.
    • (2001) Aeroelastic Behavior of Multi-Hinged Wings , pp. 449-459
    • Radcliffe, T.O.1    Cesnik, C.E.S.2
  • 9
    • 46449139779 scopus 로고    scopus 로고
    • Flutter and Divergence Analysis Using the Generalized Aeroelastic Analysis Method
    • Edwards, J.W., andWieseman, C. D., “Flutter and Divergence Analysis Using the Generalized Aeroelastic Analysis Method,” Journal of Aircraft, Vol. 45, No. 3, 2008, pp. 906–915. doi:10.2514/1.30078
    • (2008) Journal of Aircraft , vol.45 , Issue.3 , pp. 906-915
    • Edwards, J.W.1    Wieseman, C.D.2
  • 10
    • 42649135148 scopus 로고    scopus 로고
    • Two-Dimensional Incompressible Unsteady Airfoil Theory—An Overview
    • Peters, D. A., “Two-Dimensional Incompressible Unsteady Airfoil Theory—An Overview,” Journal of Fluids and Structures, Vol. 24, No. 3, 2008, pp. 295–312. doi:10.1016/j.jfluidstructs.2007.09.001
    • (2008) Journal of Fluids and Structures , vol.24 , Issue.3 , pp. 295-312
    • Peters, D.A.1
  • 13
    • 0035359418 scopus 로고    scopus 로고
    • The Quadratic Eigenvalue Problem
    • Tisseur, F., and Meerbergen, K., “The Quadratic Eigenvalue Problem,” SIAM Review, Vol. 43, No. 2, 2001, pp. 235–286. doi:10.1137/S0036144500381988
    • (2001) SIAM Review , vol.43 , Issue.2 , pp. 235-286
    • Tisseur, F.1    Meerbergen, K.2
  • 14
    • 0003199447 scopus 로고
    • The Flutter of a Uniform Cantilever Wing
    • Goland, M., “The Flutter of a Uniform Cantilever Wing,” Journal of Applied Mechanics, Vol. 12, No. 4, 1945, pp. 197–208.
    • (1945) Journal of Applied Mechanics , vol.12 , Issue.4 , pp. 197-208
    • Goland, M.1
  • 15
    • 0002406986 scopus 로고
    • The Flutter of a Uniform Cantilever Wing with Tip Weights
    • Mar
    • Goland, M., and Luke, Y. L., “The Flutter of a Uniform Cantilever Wing with Tip Weights,” Journal of Applied Mechanics, Vol. 15, No. 1, Mar. 1948, pp. 13–20.
    • (1948) Journal of Applied Mechanics , vol.15 , Issue.1 , pp. 13-20
    • Goland, M.1    Luke, Y.L.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.