Finite Element Formulation of a Three-Node Spatially Curved and Twisted Beam
A thin tailored composite wing box for a civil tiltrotor transport aircraft
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
Effect of In-Service Loads on Impact Damage Using Bi-Axial Loading