Divergence and flutter of shear deformable aircraft swept wings subjected to roll angular velocity
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Computational Mechanics
Link
http://link.springer.com/content/pdf/10.1007/s00707-009-0248-2.pdf
Reference19 articles.
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2. Goland M., Luke Y.L.: The flutter of a uniform wing with tip weights. J. Appl. Mech. 15, 13–20 (1948)
3. Librescu L.: Elastostatics and Kinetics of Anisotropic and Heterogeneous Shell-Type Structures. Noordhof International Publishers, The Netherlands (1975)
4. Housner, J.M., Stein, M.: Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings. NASA TN D-7539 (1974)
5. Lottati I.: Aeroelastic stability characteristics of a composite swept wing with tip weights for an unrestrained vehicle. J. Aircraft 24, 793–802 (1987)
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