Current economic constraints and environmental regulations call for design of more efficient
aircraft configurations. An observed trend in aircraft design to reduce the lift induced drag …

There has been a renewed interest in develo** environmentally friendly, economically
viable, and technologically feasible supersonic transport aircraft and reduced order …

In this paper, an integrated geometrically nonlinear aeroelastic framework to analyze the
static nonlinear aeroelastic response of morphing composite wing with orthotropic materials …

A theoretical nonlinear aeroelastic response analysis for a flexible high-aspect ratio wing
excited by harmonic gust load is presented along with a companion wind tunnel test. A …

Reliable aerodynamic and aeroelastic simulations of advanced aeronautical/mechanical
systems require us to predict flow-induced forces as accurately as possible. Nowadays …

Abstract An Aeroelastic-Harmonic Balance (A-HB) formulation of the Euler flow equations
using a high-order spatial discretization scheme coupled with structural dynamic equations …

Many challenges of vibration problems due to structure nonlinearity are growing while high-
aspect-ratio wings are being widely used. Feasible vibration control method is an effective …

This paper presents a new framework for corotational shell elements. The traditional
corotational formulation uses local element frames, which greatly facilitates the calculation of …

**20 年来长航时飞行的需求**烈, 大柔性飞行器的几何非线性气动弹性问题逐渐凸显,
使得气动弹性力学面临新的挑战. 本文针对大展弦比大变形的柔性飞行器 …

Dynamic modelling is a core activity in mechanical engineering towards supporting system
and control design. It is typically carried out in a computational environment, involving …