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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
Parametric Studies of Flutter Speed in a Strut-Braced Wing
On Load Updating for Finite Element Models
Computation of Actuation Power Requirements for Smart Wings With Morphing Airfoils
Influence of External Store Aerodynamics on Flutter/LCO of a Fighter Aircraft
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
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
Extension of the g-Method Flutter Solution to Aeroservoelastic Stability Analysis
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-2006-2173 Degraded Strength Prediction of Micro-Cracked Plain Woven Textile Composites
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-2006-1640 Time Domain Nonlinear Aeroelastic Analysis for HALE Wings