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Werkstoff
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Multi-objective Vibro-acoustic Optimization of Stiffened Panels Excited by Acoustic Diffuse Field
A Multi-Fidelity Multi-Strategy and Multi-Disciplinary Design Optimization Environment
Grid-Stiffened Panel Optimization Using Curvilinear Stiffeners
Karhunen-Loeve Expansion of Non-Gaussian Random Process AIAA Paper 2007-1943 CD-ROM Number 7
AIAA-2006-1961 Dynamic Fracture Analysis of Adhesively Bonded Joints Using Explicit Methods
AIAA-2006-2068 Stochastic Eigenvalue Problem with Polynomial Chaos
AIAA-2006-2168 On the Static Analysis of Sandwich Panels with Square Honeycomb Core
AIAA-2006-2173 Degraded Strength Prediction of Micro-Cracked Plain Woven Textile Composites
AIAA-2006-1640 Time Domain Nonlinear Aeroelastic Analysis for HALE Wings
AIAA-2006-1851 Flight-Loads Effects on Free-Play Induced Limit Cycle Oscillation
AIAA-2004-2004 Finite Element Load Updating for Plates
AIAA-2004-1646 Load Updating for Nonlinear Finite Element Models
AIAA-2004-1944 Nonlinear Aeroelastic Studies on a Joined-Wing with Wing Buckling Effects
AIAA-2004-1938 Nonlinear Aeroelastic Modeling by Block-Oriented Identification
Thermo-viscoelastic Analysis of Composite Plates and Shells Using a Triangular Flat Shell Element
Limit-Cycle-Oscillation Studies of a Fighter with External Stores
AIAA-2001-1295 Near-Exact Analytical Solutions to Linear Time-Variant Systems
Natural Frequencies of Thick, Generally-Laminated, Skew, Trapezoidal, Cantilever Plates
AIAA-2001-1290 Simulation of Transonic Limit Cycle Oscillations Using a CFD Time-Marching Method
Free Vibration of Thick Generally Laminated Quadrilateral Plates with Point Supports
Parallel Aeroelastic Computations by Using Coupled Euler Flow and Wing-Box Structural Models
Parametric Identification of Nonlinear Structural Dynamic Systems Using Finite Elements in Time
Integration of a Steady/Unsteady Wing-body Aerodynamic Module Into ASTROS
Hover Testing of a Smart Rotor With Induced-Strain Actuation of Blade Twist
AIAA-2001-1611 Effect of Compressive Force on Strut-Braced Wing Response
Preliminary Design of a Structural Wing-Box Under a Twist Constraint
Control Law Design in a Computational Aeroelasticity Environment
Unsteady Sonic Aerodynamics Using Acceleration Potential Approach
Nonlinear Response of Open/Closed-Loop Aeroelastic System Using a Discrete State-Space Approach