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Numerical investigation of supersonic plate flutter using the exact aerodynamic theory

โœ Scribed by V. V. Vedeneev

Book ID
110162751
Publisher
Springer
Year
2009
Tongue
English
Weight
255 KB
Volume
44
Category
Article
ISSN
0015-4628

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A variational formulation of boundary-value problems of the non-linear dynamic theory of elasticity using the Hamilton functional is presented. The quasi-static boundary-value problem for thin plates is considered. The initial system of equations, in a twodimensional formulation, is represented in t