journal article·1996-02

Supersonic flutter analysis of thermally stressed laminated composite flat panels

M. Ganapathi, M. Touratier

Composite Structures· Volume 34· Issue 2
Publisher page

Abstract

No abstract is available for this record. The assistant can identify its topic from the title, but cannot infer the study’s results.

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Research context

OpenAlex topics: Composite Structure Analysis and Optimization · Aeroelasticity and Vibration Control · Mechanical Behavior of Composites

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (19)

Show source-provided references
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8. Flutter of flat plate exposed to a nonlinear temperature distribution10.2514/3.3280 ↗
9. Flutter of thermally buckled finite element panel10.2514/3.7173 ↗
10. Finite element nonlinear panel flutter with arbitrary temperature in supersonic flow10.2514/3.11332 ↗
11. Non-linear flutter of orthotropic composite panel under aerodynamic heating10.2514/3.11798 ↗
12. A new eight node quadrilateral shear bending plate finite element10.1002/nme.1620370303 ↗
13. Ganapathi, M., Polit, O. & Touratier, M., A C∘ eight node membrane-shear-bending element for geometrically nonlinear (static and dynamic) analysis of laminates. Int. J. Numer. Meth. Engng Under review.
14. Shear correction factors for plates and shells10.1002/nme.1620330712 ↗
15. Jones · 1975
16. Piston theory — a new aerodynamic tool for the aeroelastician10.2514/8.3740 ↗
17. Comparison of panel flutter results from approximate aerodynamic theory with results from exact theory and experiment
18. Supersonic flutter of shear deformation laminated flat panel10.1016/0022-460X(90)90887-6 ↗
19. Wilkinson · 1965