Effects of geometric structural nonlinearity on flutter and limit cycle oscillations of high-aspect-ratio wings-Reference-Cited by-同舟云学术

Effects of geometric structural nonlinearity on flutter and limit cycle oscillations of high-aspect-ratio wings

Published:2004-04 Issue:3 Volume:19 Page:291-306
ISSN:0889-9746
Container-title:Journal of Fluids and Structures
language:en
Short-container-title:Journal of Fluids and Structures

Author:

Tang D.M.,Dowell E.H.

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference11 articles.

1. Convection Heat Transfer;Bejan,1984

2. Nonlinear flutter of curved plates;Dowell;AIAA Journal,1969

3. Nonlinear flutter of curved plates, Part II;Dowell;AIAA Journal,1970

4. Hodges, D.H., Dowell, E.H., 1974. Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades. NASA TN D-7818.

5. Patil, M.J., Hodges, D.H., Cesnik, C.E.S., 1999a. Limit cycle oscillations in high-aspect-ratio wings. AIAA Paper-99-1464.

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