Aerodynamic modeling plays an important role in multiphysics and design problems, in
addition to experiment and numerical simulation, due to its low-dimensional representation …

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 …

In this article the procedure and method for the ice accretion prediction for different airfoils
using artificial neural networks (ANNs) are discussed. A dataset for the neural network is …

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 …

This paper describes a methodology, called local decomposition method, which aims at
building a surrogate model based on steady turbulent aerodynamic fields at multiple …

Reduced-order modeling (ROM) commonly refers to the construction, based on a few
solutions (referred to as snapshots) of an expensive discretized partial differential equation …

A domain decomposition method which couples a high and a low-fidelity model is proposed
to reduce the computational cost of a flow simulation. This approach requires to solve the …

AIRCRAFT icing represents a serious hazard to aviation that caused many tragic fatalities
over the past decades [1]. The physical formation process of ice is affected by a variety of …

The use of non‐intrusive reduced order modeling (NIROM) to approximate high‐fidelity
computer models has been steadily increased over the past decade. Recently, local NIROM …

In this study, an ice accretion method aimed at ice crystal icing in turbofan engines is
developed and demonstrated for glaciated as well as mixed-phase icing conditions. The …