Geodesic
Flutter of a cylindrical shell subjected to an internal supersonic gas flow
Vestnik Moskovskogo universiteta. Matematika, mehanika, no. 5 (2011), pp. 61-65

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The well-known piston theory formula for the excess aerodynamic pressure is used in the majority of works devoted to the panel flutter of shells. In this paper, we consider the solution of the problem on the flutter of a cylindrical shell with internal flow by supersonic gas flow in a new formulation. 
@article{VMUMM_2011_5_a13,
     author = {A. V. Vasil'ev},
     title = {Flutter of a cylindrical shell subjected to an internal supersonic gas flow},
     journal = {Vestnik Moskovskogo universiteta. Matematika, mehanika},
     pages = {61--65},
     publisher = {mathdoc},
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     year = {2011},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/VMUMM_2011_5_a13/}
}
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A. V. Vasil'ev. Flutter of a cylindrical shell subjected to an internal supersonic gas flow. Vestnik Moskovskogo universiteta. Matematika, mehanika, no. 5 (2011), pp. 61-65. http://geodesic.mathdoc.fr/item/VMUMM_2011_5_a13/