Contemporary computational analysis of modern aircraft structures demands rapid and
efficient, yet accurate enough tools for the conceptual and preliminary design stages. On that …

This paper comprehensively reviews the progress of static aeroelastic effect prediction and
correction methods for aircraft, including the damage and protection of aeroelastic. It is …

SANDWICH panels have been the focus of numerous studies done in the past few decades
due to their high strength to weight ratio and high energy absorption characteristics. The use …

An efficient method to analyze a low-aspect-ratio composite wing with a control surface is
developed in this paper. To reduce the problem size and the computational cost, two special …

As computer power is increased, refined finite element models are employed for structural
analysis and design. However, it is still difficult and expensive to make and use refined finite …

This article presents a methodology for the detailed sizing of a composite materials aircraft
wing subject to wind tunnel testing design requirements. Aiming at the comparison among …

Structural Ritz-Based Simple-Polynomial Nonlinear Equivalent Plate Approach: An Assessment
Page 1 Structural Ritz-Based Simple-Polynomial Nonlinear Equivalent Plate Approach: An …

Cellular core structures are the state-of-the-art technology for light weight structures in the
aerospace industry. In an aerospace product, sandwich panels with cellular core represent …

COMPARED to sizing structural optimization problems, shape optimization is more complex
and more difficult to tackle. 1 Major difficulties are associated with accuracy problems in the …

Increasing aircraft performance, efficiency and safety requirements may be fulfilled, in part,
by implementing multi-disciplinary optimisation methods, including wing aeroelastic …