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A Multi-Region CFD Model for Aircraft Ground Deicing by Dispersed Liquid Spray

Energies (Basel), 2022-09, Vol.15 (17), p.6220

2022

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Heat Transfer Correlations for Smooth and Rough Airfoils

Fluids (Basel), 2023-02, Vol.8 (2), p.66

2023

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Eulerian–Lagrangian CFD model for prediction of heat transfer between aircraft deicing liquid sprays and a surface

International journal of numerical methods for heat & fluid flow, 2019-08, Vol.29 (7), p.2450-2475

2019

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CFD Model for Aircraft Ground Deicing: Verification and Validation of an Extended Enthalpy-Porosity Technique in Particulate Two Phase Flows

Fluids (Basel), 2021-06, Vol.6 (6), p.210

2021

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Surface Roughness in RANS Applied to Aircraft Ice Accretion Simulation: A Review

Fluids (Basel), 2023-10, Vol.8 (10), p.278

2023

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Data-Driven Calibration of Rough Heat Transfer Prediction Using Bayesian Inversion and Genetic Algorithm

Energies (Basel), 2022-05, Vol.15 (10), p.3793

2022

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Numerical Validation of Conjugate Heat Transfer Method for Anti-/De-Icing Piccolo System

Journal of aircraft, 2014-01, Vol.51 (1), p.104-116

2014

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Eulerian–Lagrangian CFD-microphysics modeling of a near-field contrail from a realistic turbofan

International journal of engine research, 2022-04, Vol.23 (4), p.661-677

2022

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Computational Fluid Dynamics Investigation of Transient Effects of Aircraft Ground Deicing Jets

Journal of thermophysics and heat transfer, 2019-01, Vol.33 (1), p.117-127

2019

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Sensitivity Study of Ice Accretion Simulation to Roughness Thermal Correction Model

Aerospace, 2021-03, Vol.8 (3), p.84

2021

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A Preliminary Approach towards Rotor Icing Modeling Using the Unsteady Vortex Lattice Method

Drones (Basel), 2024-02, Vol.8 (2), p.65

2024

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An Experimental Investigation of the Convective Heat Transfer on a Small Helicopter Rotor with Anti-Icing and De-Icing Test Setups

Aerospace, 2021-04, Vol.8 (4), p.96

2021

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Dynamic Moment Model for Numerical Simulation of a 6-DOF Plate Trajectory around an Aircraft

Journal of aerospace engineering, 2019-09, Vol.32 (5)

2019

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A Numerical and Experimental Investigation of the Convective Heat Transfer on a Small Helicopter Rotor Test Setup

Aerospace, 2021-02, Vol.8 (2), p.53

2021

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Predicting Maximum Lift Coefficient for Compound Wings Using Lifting Line Theory

Journal of aircraft, 2021-07, Vol.58 (4), p.717-732

2021

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Frossling Number Assessment for Airfoil Under Fully Turbulent Flow Conditions

Journal of thermophysics and heat transfer, 2022-04, Vol.36 (2), p.389-398

2022

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Predicting Rotor Heat Transfer Using the Viscous Blade Element Momentum Theory and Unsteady Vortex Lattice Method

Aerospace, 2020-07, Vol.7 (7), p.90

2020

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CFD investigation on the maximum lift coefficient degradation of rough airfoils

AIMS energy, 2021-01, Vol.9 (2), p.305-325

2021

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Parametric Studies of Flat Plate Trajectories Using VIC and Penalization

Modelling and Simulation in Engineering, 2018-01, Vol.2018, p.1-14

2018

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FENSAP-ICE's Three-Dimensional In-Flight Ice Accretion Module: ICE3D

Journal of aircraft, 2003-03, Vol.40 (2), p.239-247

2003

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Development of a Second Generation In-Flight Icing Simulation Code

Journal of fluids engineering, 2006-03, Vol.128 (2), p.378-387

2006

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Mathematical model for ice wall interactions within a level set method

International journal of engineering systems modelling and simulation, 2016, Vol.8 (2), p.125

2016

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Application of The Dual Kriging Method for The Design of Hot-Air-Based Aircraft Wing Anti-Icing System

Engineering applications of computational fluid mechanics, 2014-01, Vol.8 (4), p.530-548

2014

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Effect of Compressibility on Contrail Ice Particle Growth in an Engine Jet

International journal of turbo & jet-engines, 2014-06, Vol.31 (2)

2014

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NUMERICAL STUDY OF A HOT-AIR-BASED AIRCRAFT WING ANTI-ICING SYSTEM USING THE BOX-BEHNKEN DoE APPROACH

Transactions of the Canadian Society for Mechanical Engineering, 2013-01, Vol.37 (1), p.111-128

2013

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A Multi-Region CFD Model for Aircraft Ground Deicing by Dispersed Liquid Spray

Heat Transfer Correlations for Smooth and Rough Airfoils

Eulerian–Lagrangian CFD model for prediction of heat transfer between aircraft deicing liquid sprays and a surface

CFD Model for Aircraft Ground Deicing: Verification and Validation of an Extended Enthalpy-Porosity Technique in Particulate Two Phase Flows

Surface Roughness in RANS Applied to Aircraft Ice Accretion Simulation: A Review

Data-Driven Calibration of Rough Heat Transfer Prediction Using Bayesian Inversion and Genetic Algorithm

Numerical Validation of Conjugate Heat Transfer Method for Anti-/De-Icing Piccolo System

Eulerian–Lagrangian CFD-microphysics modeling of a near-field contrail from a realistic turbofan

Computational Fluid Dynamics Investigation of Transient Effects of Aircraft Ground Deicing Jets

Sensitivity Study of Ice Accretion Simulation to Roughness Thermal Correction Model

A Preliminary Approach towards Rotor Icing Modeling Using the Unsteady Vortex Lattice Method

An Experimental Investigation of the Convective Heat Transfer on a Small Helicopter Rotor with Anti-Icing and De-Icing Test Setups

Dynamic Moment Model for Numerical Simulation of a 6-DOF Plate Trajectory around an Aircraft

A Numerical and Experimental Investigation of the Convective Heat Transfer on a Small Helicopter Rotor Test Setup

Predicting Maximum Lift Coefficient for Compound Wings Using Lifting Line Theory

Frossling Number Assessment for Airfoil Under Fully Turbulent Flow Conditions

Predicting Rotor Heat Transfer Using the Viscous Blade Element Momentum Theory and Unsteady Vortex Lattice Method

CFD investigation on the maximum lift coefficient degradation of rough airfoils

Parametric Studies of Flat Plate Trajectories Using VIC and Penalization

FENSAP-ICE's Three-Dimensional In-Flight Ice Accretion Module: ICE3D

Development of a Second Generation In-Flight Icing Simulation Code

Mathematical model for ice wall interactions within a level set method

Application of The Dual Kriging Method for The Design of Hot-Air-Based Aircraft Wing Anti-Icing System

Effect of Compressibility on Contrail Ice Particle Growth in an Engine Jet

NUMERICAL STUDY OF A HOT-AIR-BASED AIRCRAFT WING ANTI-ICING SYSTEM USING THE BOX-BEHNKEN DoE APPROACH

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