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Werkstoff
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keywords:(Werkstoff)
Natural Frequencies of Thick, Generally-Laminated, Skew, Trapezoidal, Cantilever Plates
Parallel Aeroelastic Computations by Using Coupled Euler Flow and Wing-Box Structural Models
Hover Testing of a Smart Rotor With Induced-Strain Actuation of Blade Twist
Free Vibration of Thick Generally Laminated Quadrilateral Plates with Point Supports
Parametric Identification of Nonlinear Structural Dynamic Systems Using Finite Elements in Time
Integration of a Steady/Unsteady Wing-body Aerodynamic Module Into ASTROS
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
AIAA-2001-1290 Simulation of Transonic Limit Cycle Oscillations Using a CFD Time-Marching Method
AIAA-2001-1611 Effect of Compressive Force on Strut-Braced Wing Response
A Shear-Flexible Beam Element for Linear Analysis of Unsymmetrically Laminated Beams
Neural Networks for Inverse Problems in Damage Identification and Optical Imaging
Computation of Actuation Power Requirements for Smart Wings With Morphing Airfoils
Influence of External Store Aerodynamics on Flutter/LCO of a Fighter Aircraft
Parametric Studies of Flutter Speed in a Strut-Braced Wing
On Load Updating for Finite Element Models
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
Dynamic Stability of Laminated Composite Beams Subject to Subtangential Loads
Extension of the g-Method Flutter Solution to Aeroservoelastic Stability Analysis
Neural Networks for Inverse Problems Using Principal Component Analysis and Orthogonal Arrays
Body-Flexure Control with Smart Actuation for Hypervelocity Missiles
Effect of Compressive Force on Flutter Speed of a Strut-Braced Wing
Reliability of Laminated Composite Beams Subjected to Subtangential Loads
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
AIAA-2006-2068 Stochastic Eigenvalue Problem with Polynomial Chaos
AIAA-2006-2168 On the Static Analysis of Sandwich Panels with Square Honeycomb Core
AIAA-2006-1961 Dynamic Fracture Analysis of Adhesively Bonded Joints Using Explicit Methods
AIAA-2006-2173 Degraded Strength Prediction of Micro-Cracked Plain Woven Textile Composites
AIAA-2006-1640 Time Domain Nonlinear Aeroelastic Analysis for HALE Wings