Dynamic response of doubly curved honeycomb sandwich panels to random acoustic excitation. Part 2: Theoretical study-Reference-Cited by-同舟云学术

Dynamic response of doubly curved honeycomb sandwich panels to random acoustic excitation. Part 2: Theoretical study

Published:2003-07 Issue:3 Volume:264 Page:605-637
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

Cunningham P.R.,Langley R.S.,White R.G.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference13 articles.

1. Engineering Sciences Data Unit, Vibration and acoustic fatigue, ESDU Design Guide Series, Vols. 1–6, ESDU International, London.

2. Stresses in skin panels subjected to random acoustic loading;Clarkson;The Aeronautical Journal of the Royal Aeronautical Society,1968

3. J.E. Sweers, Prediction of response and fatigue life of honeycomb sandwich panels subjected to acoustic excitation, in: W.J. Trapp, D.M. Forney (Eds), Acoustical Fatigue in Aerospace Structures, Syracuse University Press, Syracuse, NY, 1964, pp. 389–402.

4. Random vibration analysis of stiffened honeycomb panels with beveled edges;Soovere;American Institute of Aeronautics and Astronautics Journal of Aircraft,1986

5. B.L. Clarkson, Review of sonic fatigue technology, NASA Technical Report CP-4587, 1994.

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