非定常流场降阶模型及其应用研究进展与展望 Page 1 第41 卷第6 期 力学进展 Vol. 41 No. 6
2011 年11 月25 日 ADVANCES IN MECHANICS Nov. 25, 2011 非定常流场降阶模型及其应用 …

With UAVs becoming increasingly popular in the industry, vertical take-off and landing
(VTOL) convertiplanes are emerging as a compromise between the advantages of planes …

An important prerequisite for the design, assessment and certification of aircraft and their
associated control systems is a quantitative specification of the environment in which the …

This work aims to model transonic airfoil–gust interaction and the gust response on
transonic aileron-buzz problems using high-fidelity computational fluid dynamics (CFD) and …

With the development of the large scale numerical simulation, computational fluid dynamics
and computational solid mechanics couplesimulation becomes the powerful accurate tool in …

One of the primary challenges in the study of gust encounters lies in isolating, defining, and
parametrizing a specific problem in a highly unsteady, three-dimensional, and multiscale …

NONLINEAR aeroelastic analysis is essential for high-altitude long-endurance (HALE)
aircraft. The HALE wings are likely very sizable, and hence flexible, in order to achieve the …

A new method for modeling the interaction of an aerofoil with a gust using a prescribed
velocity approach, called the split velocity method is presented. This approach effectively …

A physics-based reduced order model is presented as a viable approach to accurately
predict unsteady flowfield solutions at a fraction of the computational time that is required by …

A reduced-order model for unsteady aerodynamic calculations across a range of Mach
regimes based on linear convolution and a nonlinear correction factor is developed …