The employability of photonics technology in the modern era's highly demanding and
sophisticated domain of aerospace and submarines has been an appealing challenge for …

A meta model was developed to evaluate the performance of electrothermal anti-icing
systems for a rotorcraft engine air intake. A reduced-order model based on proper …

In this work, a numerical model for the operation of an electro-thermal Ice Protection
Systems (IPS) for an airfoil is presented. The present model solves the energy conservation …

THE ice accretion on aircraft wings and stabilizers may cause some aerodynamic
performance degradation, weight increase, control, and maneuver abilities difficulties, that …

为在飞机热气防冰系统设计过程中准确计算防护表面的防冰热载荷, 以某飞机翼段模型为例,
对防冰热载荷计算开展了研究, 给出了计算流程, 研究了来流速度, 高度, 温度 …

The icing phenomenon seriously threatens flight safety, and, therefore, the aircraft needs to
be equipped with an icing protection system. Icing may still occur when the anti-icing system …

This paper presents the implementation and results of the airfoil electrothermal anti-ice
mathematical model developed in part 1 (Silva, GA L, Silvares, OM, Zerbini …

The prevention of ice build-up on aircraft surfaces is crucial for safe operations. Thermal ice
protection systems, particularly electro-thermal systems, are commonly employed to mitigate …

电热防除/冰系统的控制涉及到电加热与外流场的传热耦合, 计算较为复杂,
可利用的数据资料较为稀少. 为探索电热防/除冰系统工作时与外流场的耦合传热规律 …

The present paper presents a validation of momentum boundary-layer integral solution and
finite-volume Reynolds-Averaged Navier Stokes (RANS) Computational Fluid Dynamics …