Icing on an aircraft is the cause of numerous adverse effects on aerodynamic performance.
Although the issue was recognized in the 1920s, the icing problem is still an area of ongoing …

The impingement and ice accretion of supercooled large droplets (SLD) on the aircraft
surface is one of the crucial factors threatening flight safety. The movement and …

A particle tracking framework for the computation of the collection efficiency for in-flight ice
accretion is presented. Algorithms for the computation of the collection efficiency are …

We propose a wing-shaped composite structure that uses an electroless nickel-plated
carbon fabric as an electro-thermal heating element, thus improving the electrical and …

Two-dimensional and quasi-3D in-flight ice accretion simulation codes have been widely
used by the aerospace industry for the last two decades as an aid to the certification …

Atmospheric icing, also called in-flight icing, is a common hazard for the operation of
uncrewed aerial vehicles (UAVs). With the background of a growing commercial and military …

Accurately predicting de-icing processes is essential to ensure the proper sizing and design
of ice protection systems in aircraft icing. A unified framework was developed to simulate an …

AIRCRAFT lift and control surfaces exposed to meteorological conditions featuring liquid
water content (LWC) in the form of supercooled droplets at temperatures below the freezing …

为预测多段翼和发动机进气道等三维复杂形状表面在结冰气象条件下的水滴撞击特性,
提出了一种基于欧拉两相流模型求解水滴收集系数的方法. 空气相和水滴相认为是单相耦合的 …

In the past two decades 2D and quasi-3D in-flight ice prediction codes have been
developed and widely used by the aerospace industry. Although efficient for calculating ice …