Seventh-Order Polynomial Constituting the Exact Buckling Mode of a Functionally Graded Column
Reinvestigation of Intuitive Approach for Thermal Postbuckling of Circular Plates
A comparative study on wind loads between design standards for the design of pipe-rack structures
A comparative study on wind loads between design standards for the design of pipe-rack structures
Structural Design Synthesis of Aircraft Engine Pylons at Certification Level of Detail
Extension of the Shear-Lag Solution for Structurally Attached Ultrasonic Active Sensors
Simultaneous Displacement and Internal Force Prescription in Shape Control of Pin-Jointed Assemblies
Improved Design Formulas for Buckling of Orthotropic Plates Under Combined Loading
Simultaneous Configuration Optimization of Multistate Reconfigurable Aerostructures
Novel Moving Isosurface Threshold Technique for Optimization of Structures Under Dynamic Loading
Coupled Aerostructural Modeling of Deployable Aerodecelerators for Mars Entry
Master Dynamic Stability Formula for Structural Members Subjected to Periodic Loads
Effective Beam Stiffness Properties of n-Strut Cylindrical Tensegrity Towers
Displacement Control of Nonlinear Pin-Jointed Assemblies Based on Force Method and Optimization
New Adaptive Technique of Kirsch Method for Structural Reanalysis
Vibration Analysis of Composite Sandwich Plates by the Generalized Differential Quadrature Method
Overview of the X-57 Structure Requirements, Modifications, and Airworthiness
Effect of Mass Variation on Vibration of a Functionally Graded Material Plate
New Methodology of Surface Mesh Geometry Design for Deployable Mesh Reflectors
Suitable Concepts for Applied Fatigue Research
Displacement Theories for In-Flight Deformed Shape Predictions of Aerospace Structures
Multiple-Surrogate Approach to Helicopter Rotor Blade Vibration Reduction
Stress-Based Optimization Method for Reproducing In-Flight Loads Using Concentrated Forces
Nonlinear Damping in Structures
Utilization of modal stress approach in random-vibration fatigue evaluation
The Satellite Attitude Simulator of the Dfvlr in Oberpfaffenhofen
Parameterization Framework for the MDAO of Wing Structural Layouts
Utilization Survey of Prototype Structural Test Article
The Vibration of a T-Shape Plates Structure
Estimation of the Reliability of Fatigue Loaded Structural Components
Control of the Flexural Axis of a Wing with Piezoelectric Actuation
Calibration of Airframe and Occupant Models for Two Full-Scale Rotorcraft Crash Tests
Light Rail Transit Car Specification Guide
The Influence of Binding on Creep-Buckling