Flutter of laminated plates in supersonic flow

A procedure has been developed for solving flutter problems of simply supported laminated plates using linear small deflection theory. The plate construction may be arbitrary as long as it satisfies the assumptions of linear small deflection theory. For such plates, the bending and extensional gover...

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Bibliographic Details
Main Author: Sawyer, James Wayne
Other Authors: Engineering Mechanics
Format: Others
Language:en_US
Published: Virginia Polytechnic Institute and State University 2019
Subjects:
Online Access:http://hdl.handle.net/10919/88687