Vibration and dynamic instability analyses of functionally graded porous doubly curved panels with piezoelectric layers in supersonic airflow
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Computational Mechanics
Link
https://link.springer.com/content/pdf/10.1007/s00707-023-03699-9.pdf
Reference75 articles.
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3. Pidaparti, R.: Flutter analysis of cantilevered curved composite panels. Compos. Struct. 25(1–4), 89–93 (1993). https://doi.org/10.1016/0263-8223(93)90154-I
4. Cunningham, P.R., White, R.G., Aglietti, G.: The effects of various design parameters on the free vibration of doubly curved composite sandwich panels. J. Sound Vib. 230(3), 617–648 (2000). https://doi.org/10.1006/jsvi.1999.2632
5. Kumar, L.R., Datta, P., Prabhakara, D.: Dynamic instability characteristics of laminated composite doubly curved panels subjected to partially distributed follower edge loading. Int. J. Solids Struct. 42(8), 2243–2264 (2005). https://doi.org/10.1142/S0219455405001507
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