On the stability of eccentrically stiffened cylindrical shells under axial compression
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Bibliographic Information
On the stability of eccentrically stiffened cylindrical shells under axial compression
（TAE report, no. 44 . Scientific report ; no. 4）
Technion- Israel Institute of Technology, Department of Aeronautical Engineering, 1965
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Note
"The research reported in this document has been sponsored by the Air Force Office of Scientific Research OAR under Grant AF EOAR 63-58 through the European Office of Aerospace Research, United States Air Force"
Bibliography: leaves 23-26
