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Werkstoff
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keywords:(Werkstoff)
Random Response Analysis of Curvilinearly-Stiffened Plate Using Element Free Galerkin Method
Supersonic Wing Box Weight Optimization Using Curvilinear Spars and Ribs (SpaRibs)
A Ritz Approach for Buckling Prediction of Cracked-Stiffened Structures
A Review of Soft Body Impact on Composite Structure
ZEUS-DO: Design Oriented CFD-Based Unsteady Aerodynamics for Flight Vehicle Shape Optimization
Parameterization of Curvilinear Spars and Ribs (SpaRibs) for Optimum Wing Structural Design
Development of Framework for Truss-Braced Wing Conceptual MDO
A Modified Dynamic Preisach Model for Hysteresis
Buckling and Stress Analysis of Curvilinearly Stiffened Plates Using Meshfree Method
Durable Joining Technology for Uniformly-Curved Composite Sandwich Structures
Algorithm Development for Optimization of Arbitrary Geometry Panels Using Curvilinear Stiffeners
Random Crack Propagation Analysis of a Beam with a Crack
Compression After Impact on Honeycomb Core Sandwich Panels with Thin Facesheets, Part 2: Analysis
A Multidisciplinary Analysis Optimization Environment for Wings Having SpaRibs
Micro-Structural Modeling of 2-D Plain Woven Textile Composites
Studies of Aerodynamic Influence of Under-Wing Stores on Flutter Characteristics of F-16
A POD-based Reduced Order Design Scheme for Shape Optimization of Air Vehicles
Progressive Failure Analysis of Laminated Composite Structures Based on Puck's Failure Criteria
Flutter Modeling and Suppression for a Strut-Braced Wing
Behavior of Epoxy Nanocomposites under the Vacuum Ultraviolet Irradiation
Vibration of Plate with Curvilinear Stiffeners Using Meshfree Method
Stiffener Effectiveness Approach for Optimal Stiffener Placement on Curvilinear Stiffened Panel
Continuous Dynamic Simulation for Morphing Wing Aeroelasticity
Dynamic Nonlinear Aeroelastic Analysis of the Joined Wing Configuration
Design Optimization for Minimum Sound Radiation from Point-Excited Curvilinearly Stiffened Panel
Extension of MSC Nastran UVLM.OpenFSI for Rotational Applications Including Wind Turbines
Compression After Impact on Honeycomb Core Sandwich Panels with Thin Facesheets, Part 1: Experiments
Structural Design of a Truss Braced Wing: Potential and Challenges
Buckling and Crack Propagation of Cracked Box Beams
Enabling Sensitivity Analysis Capability for a CFD-Based Unsteady Aerodynamic/Aeroelastic Solver
Integrated Local Petrov-Galerkin Sinc Method for Structural Mechanics Problems
Development of Framework for the Design Optimization of Unitized Structures
Aeroelastic Analysis and Optimization of a Rigid/Inflatable Wing
Damage Detection in a Prestressed Membrane Using a Wavelet-Based Neuro-Fuzzy System
Optimization of Unitized Structures Under Damage Tolerance Constraints
Flow Induced Vibrations of Pressure/Temperature Sensors
Generalized Linear Random Vibration Analysis Using Auto-Covariance Orthogonal Decomposition
Structural and Aeroelastic Characteristics of Truss Braced Wings: A Parametric Study