Divergence and flutter of shear deformable aircraft swept wings subjected to roll angular velocity-Reference-Cited by-同舟云学术

Divergence and flutter of shear deformable aircraft swept wings subjected to roll angular velocity

Published:2009-11-11 Issue:1-2 Volume:212 Page:151-165
ISSN:0001-5970
Container-title:Acta Mechanica
language:en
Short-container-title:Acta Mech

Author:

Fazelzadeh S. Ahmad,Marzocca P.,Mazidi A.,Rashidi E.

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.

1. Goland M.: The flutter of a uniform cantilever wing. J. Appl. Mech. 12, 197–208 (1945)

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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