Results 31 to 40 of about 2,085,127 (180)

A New Ice Accretion Model for Aircraft Icing Based on Phase-Field Method

open access: yesApplied Sciences, 2021
Aircraft icing presents a serious threat to the aerodynamic performance and safety of aircraft. The numerical simulation method for the accurate prediction of icing shape is an important method to evaluate icing hazards and develop aircraft icing ...
Hao Dai   +3 more
doaj   +1 more source

Numerical Simulation of Ice Crystal Supercooled Droplet Mixed Phase Icing Based on the Improved Messinger Model

open access: yesInternational Journal of Aerospace Engineering, 2023
The ice crystal supercooled droplet mixed phase icing problem is an important research direction in aircraft icing and has received more attention in recent years.
Zhengzhi Wang   +4 more
doaj   +1 more source

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

open access: yesAerospace, 2021
Successful icing/de-icing simulations for rotorcraft require a good prediction of the convective heat transfer on the blade’s surface. Rotorcraft icing is an unwanted phenomenon that is known to cause flight cancelations, loss of rotor performance and ...
Abdallah Samad   +4 more
doaj   +1 more source

Numerical and Experimental Investigation of the Design of a Piezoelectric De-Icing System for Small Rotorcraft Part 3/3: Numerical Model and Experimental Validation of Vibration-Based De-Icing of a Flat Plate Structure

open access: yesAerospace, 2020
The objective of this research project is divided in four parts: (1) to design a piezoelectric actuator-based de-icing system integrated to a flat plate experimental setup and develop a numerical model of the system with experimental validation, (2) use ...
Eric Villeneuve   +2 more
doaj   +1 more source

Spontaneous dewetting transitions of droplets during icing & melting cycle

open access: yesNature Communications, 2022
Despite promising for anti-icing applications, structured superhydrophobic surfaces usually lose their hydrophobicity after a few icing/melting cycles.
Lizhong Wang   +7 more
doaj   +1 more source

Numerical and Experimental Investigation of the Design of a Piezoelectric De-Icing System for Small Rotorcraft Part 1/3: Development of a Flat Plate Numerical Model with Experimental Validation

open access: yesAerospace, 2020
The objective of this research project is divided in four parts: (1) to design a piezoelectric actuator-based de-icing system integrated to a flat plate experimental setup and develop a numerical model of the system with experimental validation, (2) use ...
Eric Villeneuve   +2 more
doaj   +1 more source

Salient Object Detection Method Based on Multi-scale Visual Perception Feature Fusion [PDF]

open access: yesJisuanji kexue
Salient object detection has important theoretical research significance and practical application value,and has played an important role in many computer vision applications,such as visual tracking,image segmentation and object recognition.How-ever,the ...
WU Xiaoqin, ZHOU Wenjun, ZUO Chenglin, WANG Yifan, PENG Bo
doaj   +1 more source

Determination of anti-icing properties of a gas-thermal coating protective coating with a surface layer of PTFE [PDF]

open access: yesE3S Web of Conferences, 2023
Icing is a negative factor in the operation of various structures and equipment. Ice, due to its physical characteristics, has an aggressive effect on the surfaces of many materials.
Kostin Vasily   +4 more
doaj   +1 more source

Effect of Various Surface Coatings on De-Icing/Anti-Icing Fluids Aerodynamic and Endurance Time Performances

open access: yesAerospace, 2019
The Anti-icing Materials International Laboratory (AMIL) has been testing SAE AMS1424 and AMS1428 ground de-icing/anti-icing fluids for more than 30 years.
Eric Villeneuve   +2 more
doaj   +1 more source

The quality evaluation of aero-thermal flowfield in 0.75m × 0.50m icing wind tunnel

open access: yesHangkong gongcheng jinzhan
The quality of aero-thermal flowfield of the icing wind tunnel is the precondition for its experimental application. In order to evaluate the quality of the aerodynamic flowfield and the thermodynamic flowfield of 0.75 m × 0.50 m icing wind tunnel, the ...
WEI Longtao   +3 more
doaj   +1 more source

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