This paper deals with a theoretical analysis of the dynamic response of shear deformable symmetrically laminated rectangular composite flat panels exposed to sonic boom and explosive blast loadings. The pertinent governing equations incorporating transverse shear deformation, transverse normal stress, as well as the higher-order effects are solved by using the integral-transform technique. The obtained results are compared with their counterparts obtained within the framework of the first-order transverse shear deformation and the classical plate theories and some conclusions concerning their range of applicability are outlined. The paper also contains a detailed analysis of the influence played by the various parameters characterizing the considered pressure pulses as well as the material and geometry of the plate.
Response of laminated composite flat panels to sonic boom and explosive blast loadings
AIAA Journal ; 28
1990-02-01
Sonstige
Keine Angabe
Englisch
Dynamic Multimode Response of Composite Plates to Sonic Boom and Blast Loadings
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