Behavior of plate strip under shear and compressive stresses beyond buckling limit.

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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.], 1938.
Subjects:	Mathematical models. Aeronautics > Research. Airplanes.

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Full Text (via ProQuest)

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Call Number:	Y3.N21_5..8_870
Y3.N21_5..8_870	Available