A Transform Potential Theoretic Method for Acoustic Radiation from Structures
Parallel Numerical Simulation on Crack Propagation of Aeronautical Structures
EAP Actuators for Controlling Space Inflatable Structures
Stochastic Analysis of Nonlinear Viscoelastic Panels Under Random Excitation
Analysis of Nonstationary Vibroacoustic Flight Data Using a Damage-Potential Basis
Need for Combining Space Law with Environmental Law and Global Federalism
Development of an Adaptive Passive Vibro-Acoustic Device for Payload Fairings
Characterization and Modeling of the Fracture Behavior of Epoxy Nanocomposites
Challenges to Space Law in the 21st Century - Project 2001 Plus
A Comparison of Recovery Methods for Reduced Dynamic Substructure Models with Internal Loads
A Robust Algorithm for the Automated Design of Steel Structures
The Impact of Arms Limitation Agreements and Export Control Regulations on Launch Activities
Preliminary Design of a Structural Wing-Box Under a Twist Constraint
Development of a High Accuracy MEMS Angular Measurement System for Hypersonic Wind Tunnel Facilities
Instrumentation of an F-16 Wing Pylon for In-flight Monitoring of Store Loads
Carbon-Nanotube-Reinforced Structural Materials and Nonequilibrium Thermodynamic Models
Helicopter Performance and Vibration Enhancement by Twist-Actuated Blades
Electromechanical Modeling of a Piezoelectric Actuator for Modulated/Vectored Blowing
Curvilinear Fiber Design of Composite Laminae by Cellular Automata
Probabilistic Design of Aerospace Vehicles: Coupling Global and Local Requirements
Mixed Discrete Synthetic Approach for Nonlinear Design Optimization
Optimization Based Efficiencies in First Order Reliability Analysis
Optimal Overload Ratio Age Dependency in Fatigue Crack Growth
Flutter Suppression Using Micro-Trailing Edge Effectors
Three-Dimensional Post-buckling Analysis of Highly Flexible Curved Beams
Design of Multi-Degree-of-Freedom Tuned-Mass Dampers Based on Eigenvalue Perturbation
A Fuzzy Approach to Fiber-Reinforced Composite Material Mechanics
Modeling of Crack Opening Displacement due to Delamination Using First-order Shear Laminate Theory
Force Identification in a FGM Plate Using Truncated Response
Elasticity Analysis and Optimization of a Functionally Graded Plate with Hole
Computational Modeling of Progressive Damage in Composite Laminates
A New Approach to Aeroservoelastic Aircraft Modelling
A State Transition Approach to Reliability Based Design and Optimization
Mode I Fracture of Polymer Matrix Composites to -269^oC