AIAA-2001-1517 A Large Deformation Viscoelastic Model with Fractional Order Rate Laws
AIAA-2001-1498 Sequential Multipoint Quadratic Approximation for Numerical Optimization
AIAA-2001-1442 Recent Advances in Active Damage Interrogation
AIAA-2001-1440 Reliable Adaptive Structures via Sensor Integration: Research and Development Issues
AIAA-2001-1425 Error Budgeting for Assembly-Centric Design of Aerostructures
AIAA-2001-1385 CASTOR Experiment Results
AIAA-2001-1382 MPLM On-Orbit Interface Dynamic Flexibility Modal Test
AIAA-2001-1347 The Constitutive Modeling of Thin Films with Random Material Wrinkles
AIAA-2001-1345 Thin Film Membrane Wrinkling Due to Mechanical and Thermal Loads
AIAA-2001-1336 Stiffness Evaluation of Elliptical Laminated Composite Tube Under Bending
AIAA-2001-1318 Probabilistic Modal Analysis for Turbine Engine Blades
AIAA-2001-1255 10 Million DOF Finite Element Structural Analysis via Internet Super-Computing
AIAA-2001-1252 Two Dimensional Contact of Dissimilar/Anisotropic Materials
AIAA-2001-1251 A New Frictional Contact Problem Formulation Using Augmented Lagrangian Method
AIAA-2001-1250 Singularities of Multimaterial Wedges in Heterogeneous Structures
AIAA-2001-1212 Transonic Limit Cycle Oscillation Analysis Using Reduced Order Aerodynamic Models
AIAA-2001-1205 Composite Wing Structural Design Optimization with Continuity Constraints
AIAA-2001-1184 Strain Invariant Failure Criteria for Polymers in Composite Materials
AIAA-2001-1674 Comparison and Combination of Two Different Lifting Methods: Fatigue and Statistics
AIAA-2001-1659 Nonlinear Response of Thermal Protection System at Supersonic Speeds
AIAA-2001-1630 Structural Design Process Improvement Using Evolutionary Finite Element Models
AIAA-2001-1623 Analytical Expressions of Sensitivities for Shape Variables in Linear Bending Systems
AIAA-2001-1622 Adaptive Experimental Design for Construction of Response Surface Approximations
AIAA-2001-1605 Using a Genetic Algorithm for Structural Topology Design of Helicopter Rotor Blades
AIAA-2001-1602 Impact Test and Simulation of Energy Absorbing Concepts for Earth Entry Vehicles
AIAA-2001-1587 Vibroacoustic Model Validation for a Curved Honeycomb Composite Panel
AIAA-2001-1545 Stable Damage Growth in Composite Sandwich Panels Under Static Compression
AIAA-2001-1518 A Possibilistic Approach for General Design Optimization Problems
AIAA-2001-1490 Optimum Design for Double-Lap Bolted Composite Joints Using a Genetic Algorithm
AIAA-2001-1478 Building Blocks of Large Deployable Precision Membrane Reflectors
AIAA-2001-1411 Mode Splitting in an Inflated Polyimide Cylinder with Circumferential Asymmetry
AIAA-2001-1396 The Prerequisites for an Advanced Design Methodology in Shells Prone to Buckling
AIAA-2001-1392 On a High-Fidelity Hierarchical Approach to Buckling Load Calculations
AIAA-2001-1391 Dynamics of Damaged Plates
AIAA-2001-1390 Bird Impact Simulation Against a Hybrid Composite and Metallic Vertical Stabilizer
AIAA-2001-1367 Surface Modification of IM7/5260 Composites by NF3 DC-Plasma
AIAA-2001-1344 Shape Characteristics of Spin-Stabilized Structures under Microgravity Environment
AIAA-2001-1332 Anisotropy Induced Spiral Buckling in Cylindrical Shells