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+keyword:(spacecraft structures)
AIAA-2001-1255 10 Million DOF Finite Element Structural Analysis via Internet Super-Computing
AIAA-2001-1256 Node Activation Technique for Finite Element System
AIAA-2001-1570 Virtual Experimental Characterization of 3D Orthogonal Woven Composite Materials
AIAA-2001-1474 Parallel Algorithm to Solve One Million DOF Eigenvalue Problem by PCs
AIAA-2001-1202 Simultaneous Optimization of Design and Manufacture of Composite Structures
Dynamic Analysis for Delaminated Composites Using DKQ Concept Based on Higher-Order Zig-Zag Theory
Effect of Unsteady Blade Motion on the Aerodynamic Performance of Micro-Rotorcraft
Active Load Control of an Articulated Composite Rotor Blade via Dual Trailing Edge Flaps
Spectral Element Model for the Vibration of an Axially Moving Timoshenko Beam
Transonic/Supersonic Aeroelastic Instability of an All Movable Wing with Structural Nonlinearity
Design and Performance Tests of Cycloidal Propulsion Systems
Parallel Numerical Simulation on Crack Propagation of Aeronautical Structures
Comparative Study on Vibration Control Methodologies Applied to Adaptive Anisotropic Cantilevers
Finite Element Analysis by Piggyback Concept in Distributed Computing Environment
Three Dimensional Stress Analysis by Node Activation Method