Buckling and Vibrations of Periodically Supported Non-Prismatic Columns using an Integral Equation Approach
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University
Publisher
American Institute of Aeronautics and Astronautics
Reference17 articles.
1. Engineering Series;Timoshenko S.,1961
2. Stroud, W. J., Greene, W. H., and Anderson, M. S. “Deflections of Beam Columns on Multiple Supports. [Shuttle Thermal Protection System],” Technical Report NASA-TM-81829, NASA Langley Research Center; Hampton, VA, United States,1980.
3. Thermal buckling analysis of periodically supported composite beams using Isogeometric analysis
4. Estimation of Launch Vehicle Propellant Tank Structural Weight Using Simplified Beam Approximation
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