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Werkstoff
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Adapted K-Method for Frequency-Domain ASE Control Stability Margin Analysis (AIAA 2014-1198)
A Review of Soft Body Impact on Composite Structure
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
ZEUS-DO: Design Oriented CFD-Based Unsteady Aerodynamics for Flight Vehicle Shape Optimization
Nonlinear Aeroelastic Analysis for A Wrinkling Aeroshell/Ballute System
Durable Joining Technology for Uniformly-Curved Composite Sandwich Structures
Random Crack Propagation Analysis of a Beam with a Crack
Development of Framework for Truss-Braced Wing Conceptual MDO
Algorithm Development for Optimization of Arbitrary Geometry Panels Using Curvilinear Stiffeners
Compression After Impact on Honeycomb Core Sandwich Panels with Thin Facesheets, Part 2: Analysis
A Nested Extreme Response Surface Approach for RBDO with Time-Dependent Probabilistic Constraints
A Multidisciplinary Analysis Optimization Environment for Wings Having SpaRibs
Parameterization of Curvilinear Spars and Ribs (SpaRibs) for Optimum Wing Structural Design
Behavior of Epoxy Nanocomposites under the Vacuum Ultraviolet Irradiation
A Modified Dynamic Preisach Model for Hysteresis
Buckling and Stress Analysis of Curvilinearly Stiffened Plates Using Meshfree Method
Studies of Aerodynamic Influence of Under-Wing Stores on Flutter Characteristics of F-16
Enhanced Bi-Level Integrated System Synthesis 2000 (Ebliss 2000)
Flutter Modeling and Suppression for a Strut-Braced Wing
Vibration of Plate with Curvilinear Stiffeners Using Meshfree Method
Stiffener Effectiveness Approach for Optimal Stiffener Placement on Curvilinear Stiffened Panel
Design Optimization for Minimum Sound Radiation from Point-Excited Curvilinearly Stiffened Panel
Micro-Structural Modeling of 2-D Plain Woven Textile Composites
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
Buckling and Crack Propagation of Cracked Box Beams
Enabling Sensitivity Analysis Capability for a CFD-Based Unsteady Aerodynamic/Aeroelastic Solver
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
Continuous Dynamic Simulation for Morphing Wing Aeroelasticity
Dynamic Nonlinear Aeroelastic Analysis of the Joined Wing Configuration
Structural Design of a Truss Braced Wing: Potential and Challenges
Nonlinear Aeroelastic Methodology for a Membrane-on-Ballute Model with Hypersonic Bow Shock
Aeroelastic Analysis and Optimization of a Rigid/Inflatable Wing
Integrated Local Petrov-Galerkin Sinc Method for Structural Mechanics Problems
Development of Framework for the Design Optimization of Unitized Structures
A Compact CFD-Based Reduced Order Modeling for Gust Analysis