An Experimental Study on Ice Accretion and Anti-/De-Icing of a Pitot Tube

2022 ◽  
Author(s):  
Haiyang Hu ◽  
Faisal Al-Masri ◽  
Hui Hu
Keyword(s):  
Experimental Study ◽  
Pitot Tube ◽  
Ice Accretion

scholarly journals 3D RECONSTRUCTION OF ICE SHAPE USING VISIBLE AND THERMAL RANGE IMAGING FOR AIRCRAFT ICING STUDY

2021 ◽  
Vol XLIII-B2-2021 ◽  
pp. 527-532
Author(s):  
V. A. Knyaz ◽  
E. V. Ippolitov ◽  
M. M. Novikov
Keyword(s):  
Experimental Study ◽  
Aerodynamic Characteristics ◽  
Physical Models ◽  
Accurate Information ◽  
Ice Accretion ◽  
Aircraft Icing ◽  
Thermal Range ◽  
Quantitative Understanding ◽  
Behaviour Study ◽  
Different Levels

Abstract. Aircraft icing is one of the main factors decreasing the flight safety. Qualitative and quantitative understanding of the icing process is crucially needed for developing anti-icing measures and safety recommendations. Changes in aerodynamic characteristics of aircraft caused by changes in shape of aircraft surfaces due to the ice accretion can lead to significant aerodynamic performance degradation. So the reliable and accurate information of how the shape of the ice accretion influences on aerodynamic characteristics is a key point for predicting the changes in aerodynamic performance.The study addresses to a problem of accurate shape measuring of ice accretion for further experimental study of iced-aircraft aerodynamic in a hydrodynamic tunnel. For this purpose the evaluation of various techniques of ice 3D measurements is performed that include as visible so thermal imaging of ice accretion. The results of evaluation serves for the decision of preferable technique to be used in experimental study. Also the framework is developed for creating physical models of iced aircraft based on result of real ice accretion shape measurement. It allows to produce stereolithography (SLA) copies of of an aircraft under icing condition for different levels of icing. These SLA-models of an aircraft under icing condition are then used for flow behaviour study in order to identify critical flying condition.

An experimental study on mitigating dynamic ice accretion process on bridge cables with a superhydrophobic coating

2022 ◽  
Vol 132 ◽  
pp. 110573
Author(s):  
Yihua Peng ◽  
Ramsankar Veerakumar ◽  
Zichen Zhang ◽  
Haiyang Hu ◽  
Yang Liu ◽  
...  
Keyword(s):  
Experimental Study ◽  
Ice Accretion ◽  
Superhydrophobic Coating ◽  
Accretion Process

307 Experimental Study of Ice Accretion on Axial Fan

2012 ◽  
Vol 2012.51 (0) ◽  
pp. 87-88
Author(s):  
Hiroyuki Maki ◽  
Riho HIRAMOTO ◽  
Hiroaki KAWAI ◽  
Syouta YAMADA ◽  
Yuuki KOUEN
Keyword(s):  
Experimental Study ◽  
Ice Accretion ◽  
Axial Fan

Experimental Study of Splitting Device for Horizontal Pipeline

2014 ◽  
Vol 660 ◽  
pp. 714-718
Author(s):  
Norasikin Mat Isa ◽  
A. Malek Izzat ◽  
Azmahani Sadikin ◽  
Siti Mariam Basharie ◽  
Nor Zelawati Asmuin
Keyword(s):  
Experimental Study ◽  
Velocity Profile ◽  
Qualitative Analysis ◽  
Flow Distribution ◽  
Pitot Tube ◽  
Scale Model ◽  
Homogeneous Flow ◽  
Airflow Distribution ◽  
And Behavior ◽  
Reduced Scale

The flow distribution within a reduced scale model pipeline to study and determine the best splitting device for a horizontal pipeline through experiments were conducted. In this research, five splitting devices are designed and tested on the model rig. Out of five, only one splitting device has been chosen that achieved the objective the best; to improve airflow to be a homogeneous flow in the pipe, or at least reducing and improving from the roping condition. The process of selecting the best device had been done through qualitative analysis of velocity profile and airflow distribution obtained from Pitot Tube measurements, besides the airflow pattern and behavior through PIV results.

Sign in / Sign up

Export Citation Format

Share Document