A method of estimating the critical buckling load for structural members.

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Bibliographic Details
Online Access: Full Text (via ProQuest)
Corporate Author: United States. National Advisory Committee for Aeronautics
Format: Government Document eBook
Language:English
Published: [Washington] : [s.n.], 1939.
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Call Number: Y3.N21_5..6_717
Y3.N21_5..6_717 Available