Shape sensitivity analysis of flutter response of a laminated wing
Computation of actuation power requirements for smart wings with morphing airfoils
Analysis of a Thin-walled Beam with a Crack of Random Location and Size
Global/Local Optimization of Aircraft Wing Using Parallel Processing
The structural optimization of a cantilever aircraft wing with stiffeners and curvilinear spars and ribs is described. The decomposition
...Vibration Analysis of Curvilinearly Stiffened Composite Panel Subjected to In-Plane Loads
This paper presents an efficient finite element approach to study the prestressed vibration mode results of a curvilinearly stiffened
...Rapid Transonic Flutter Analysis for Aircraft Conceptual Design Applications
This paper studies weight minimization of a composite flying-wing aircraft using bioinspired arbitrarily shaped spars and ribs, known as
...Controllability Gramian as Control Design Objective in Aircraft Structural Design Optimization
Nonintrusive Computation of Rigid-Body/Flexible-Body Coupling Integrals
Failure of Hexagonal and Triangular Honeycomb Core Sandwich Panels
Skin-Stringer Assembly Using Radial Basis Functions for Curvilinearly Stiffened Panels
Additive manufacturing enables the deposition of material in the near-net shape at any desired location on the base plate or shell to
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