Geodesic
Finite-element solution of panel flutter of shell structures
Matematičeskoe modelirovanie, Tome 14 (2002) no. 12, pp. 55-71

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The finite-element algorithm is described to solve the problem of the panel flutter of multilayer loaded/unloaded shell structures subjected to the action of external or internal supersonic gas flow. Some aspects of numerical realization of this algorithm are considered. Calculation results are presented. 
@article{MM_2002_14_12_a5,
     author = {S. A. Bochkarev and V. P. Matveenko},
     title = {Finite-element solution of panel flutter of shell structures},
     journal = {Matemati\v{c}eskoe modelirovanie},
     pages = {55--71},
     publisher = {mathdoc},
     volume = {14},
     number = {12},
     year = {2002},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/MM_2002_14_12_a5/}
}
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S. A. Bochkarev; V. P. Matveenko. Finite-element solution of panel flutter of shell structures. Matematičeskoe modelirovanie, Tome 14 (2002) no. 12, pp. 55-71. http://geodesic.mathdoc.fr/item/MM_2002_14_12_a5/