Aeronautical Quarterly · 1954 · 51 citations · 0 references
EngineeringCivil EngineeringMechanical Behavior Of MaterialsStructural AnalysisStructural EngineeringBuckling AnalysisElastic DeformationPlate AnalysisPlate TheoryStress AnalysisStructural MechanicsAxial CompressionBuckling Of Rectangular PlatesBuckling Under Axial CompressionCompressionOrthotropic Plate AnalysisOrthotropic Plate TheoryPlate BucklingPlate Buckling Analysis
Summary Four buckling problems are considered, namely: — (a) A rectangular orthotropic plate, with all edges simply supported, subjected to compression on its ends and a known compression or tension on its sides; (b) the same as (a) but with the ends clamped and sides simply supported; (c) a rectangular orthotropic plate, with the ends simply supported and sides clamped, subjected to compression on its ends; and (d) the same as (c) but with all edges clamped. In each case it is shown that the variables involved can all be combined into such a non-dimensional form that a single curve serves to give the value of the end compression required to cause buckling. This curve is identical with the curve of buckling stress coefficient against side ratio for a corresponding isotropic plate under uni-axial compression.