Finite Element Formulation of a Three-Node Spatially Curved and Twisted Beam
A Thin Tailored Composite Wing Box for a Civil Tiltrotor Transport Aircraft
An Overview of the Advanced Lightweight Aircraft Fuselage Structures (ALAFS) Program
An overview of the advanced lightweight aircraft fuselage structures (ALAFS) program
Optimization of Structures Designed Using Nonlinear FEM Analysis
A Model Modification Method Using Perturbed Finite Elements
Probabilistic assessment of multiple site damage in aircraft structures
Probabilistic Assessment of Multiple Site Damage in Aircraft Structures
Effect of In-Service Loads on Impact Damage Using Bi-Axial Loading
Broadband Vibration Damping in Beams Using Distributed Viscoelastic Tuned Mass Absorbers
Constrained Optimization of Thin-Walled Composite Beams with Coupling
Transmission of Stochastic Pressures Through an Aeroelastic Plate into a Cavity
Development of a pressure box to evaluate reusable-launch-vehicle cryogenic-tank panels
Development of a Pressure Box to Evaluate Reusable-Launch-Vehicle Cryogenic-Tank Panels
Strategy for Modeling Eight-Harness Satin Weave Carbon/Carbon Composites Subjected to Thermal Loads
V-Lab: A Virtual Laboratory for Structural Integrity Assessment of Composite Components