Continuous Tow Steering Around an Elliptical Cutout in a Composite Panel
General Closed-Form Solution of Piecewise Circular Frames of Aircraft
Ritz Solution for Transient Analysis of Variable-Stiffness Shell Structures
Free Vibration of Thick Quadrilateral Laminates Using Third-Order Shear-Normal Deformation Theory
Lowest Twelve Frequencies of Sandwich Plates Using Third-Order Shear-Normal Deformation Theory
MAI Form : Schlussbericht : Laufzeit des Vorhabens: 01/11/2014 bis 30/04/2017
MAI Form : Schlussbericht : Laufzeit des Vorhabens: 01/11/2014 bis 30/04/2017
Nonlinear Modal Interactions of Swept Composite Aircraft Wings Carrying External Stores
Improved Finite Element Method for Inflated Beams with Local Wrinkles
Micromechanics Models for Viscoelastic Plain-Weave Composite Tape Springs
Fatigue Life Improvement for Aeroengine Disks Based on Active Thermal Management
Reduced-Order Models for a Shallow Curved Beam Under Combined Loading
Effect of Mass Variation on Vibration of a Functionally Graded Material Plate
Topology and Shape Optimization of Ultrathin Composite Self-Deployable Shell Structures with Cutouts
Nonlinear Buckling and Postbuckling Analysis of Tow-Steered Composite Cylinders with Cutouts