Hybrid finite element method applied to supersonic flutter of an empty or partially liquid-filled truncated conical shell
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics
Reference26 articles.
1. Finite elements in aeroelasticity of plates and shells;Bismarck-Nasr;Applied Mechanics Reviews,1996
2. Aeroelasticity of Plates and Shells;Dowell,1975
3. Supersonic flutter of circular cylindrical shells subjected to internal pressure and axial compression;Olson;AIAA Journal,1966
4. Comparing theory and experiment for supersonic flutter of circular cylindrical shells;Olson;AIAA Journal,1967
5. Aeroelastic stability characteristics of cylindrical shells considering imperfections and edge constraint;Barr;AIAA Journal,1969
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