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Investigation on nonlinear buckling performance of the optimized wing structure under the realistic flight cases

Ke Liang, Zhen Yin

2023Aerospace Science and Technology11 citationsDOI

Topics & Concepts

BucklingWingStructural engineeringNonlinear systemFinite element methodAerodynamicsFlight dynamicsCritical loadInstabilityBoundary value problemEngineeringAerospace engineeringMechanicsMathematicsPhysicsMathematical analysisQuantum mechanicsAeroelasticity and Vibration ControlComposite Structure Analysis and OptimizationProbabilistic and Robust Engineering Design
Investigation on nonlinear buckling performance of the optimized wing structure under the realistic flight cases | Litcius