The Aeronautical Journal · 1969 · 31 citations · 0 references
EngineeringAerospace EngineeringMechanical EngineeringAircraft StructuresStructural AnalysisStructural EngineeringBuckling AnalysisBuckling Of Aircraft StructuresPlate AnalysisPlate TheoryStructural MechanicsThermal StressesBuckling Of Rectangular PlatesPanel BucklingPlate BucklingPlate Buckling AnalysisResidual Thermal StressesThermal BucklingThermal Buckling AnalysisTransient Thermal Stresses
Circumstances can arise in which a rectangular panel, forming part of a structure, is subject to non-uniform in-plane compression, and in which it is important that instability of the panel should not occur. Problems of this nature occur, for example, in the structure of modern highspeed aircraft subject to the transient thermal stresses that can arise from rapid changes of speed or altitude.