Aircraft structures experience various kinds of loads over their entire lifetime, typically
leading to fatigue, and ultimately structural failure. To avoid structural failure during …

In this work, a new approach for the generation of a generalized state-space
aeroservoelastic model based on tangential interpolation is presented. The resulting system …

The design process for new aircraft configurations is complex, very costly and many
disciplines are involved, like aerodynamics, structure, loads analysis, aeroelasticity, flight …

The paper addresses the application of a parametric design process for a flying wing
configuration. The multi-disciplinary configuration (MULDICON) is a generic unmanned …

The Loads Kernel Software allows for the calculation of quasi-steady and dynamic
maneuver loads, unsteady gust loads in the time and frequency domain as well as dynamic …

摘暋要: 由于技术条件和飞机研制周期限制, 结构强度计算的载荷设计情况必须进行筛选,
因此有必要对结构部件总载荷, 简化工程梁内载荷分布的包络线进行研究 …

MANY methodologies (see [1–4]) have been proposed to quickly identify among a very large
number of flight conditions and maneuvers (ie, steady, quasi-steady, and unsteady load …

Using a flexible airframe model, this study optimizes various single-port (two-terminal)
passive mechanical networks that consist of an arrangement of springs, dampers, and …

Airframe flexibility effects have typically been captured by modal reduction of the airframe.
Although efficient, this model may still be prohibitively expensive for preliminary design …

Aircraft structures experience various kinds of loads over their entire lifetime, typically
leading to fatigue and ultimately structural failure. In order to avoid structural failure during …