Integrating Ice Protection and Noise Abatement Systems for Aircraft Application: A Review

被引:1
|
作者
Munas, Fathima Rehana [1 ,2 ]
Hwa, Yu Kok [1 ]
Yusoff, Norwahida [1 ]
Muzathik, Abdul Majeed [2 ]
Ismail, Mohd Azmi [1 ]
机构
[1] Univ Sains Malaysia, Sch Mech Engn, Engn Campus, Nibong Tebal 14300, Penang, Malaysia
[2] South Eastern Univ Sri Lanka, Dept Mech Engn, Fac Engn, Oluvil 32360, Eastern Provinc, Sri Lanka
来源
关键词
Acoustic liner; bias acoustic liner; ice protection; noise abatement; NUMERICAL-SIMULATION; HEAT-TRANSFER; ACCRETION;
D O I
10.47836/pjst.31.6.02
中图分类号
O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];
学科分类号
07 ; 0710 ; 09 ;
摘要
Aircraft icing remains a key aviation hazard as the global fleet of aircraft in various sectors continues to expand, posing a serious threat to flight safety. As previously stated, the growth of this type of aircraft has been accompanied by an increase in noise levels, and aircraft is reportedly the second most bothersome noise source after traffic. However, integrating an acoustic liner with anti-icing techniques on the leading edge of a nacelle would not efficiently eliminate forward radiated noise and improve the thermal performance of the anti-icing system. Hence, it is of the utmost importance to research the integration of ice protection and noise abatement systems for aircraft applications. This review discusses the integration of ice accretion and noise abatement systems in aircraft applications. The prominence of this review is to explain significant features such as ice protection systems, Computational Fluid Dynamics in ice protection, noise abatement systems, and the integration of ice protection systems and noise abatement systems wherever they are described.
引用
收藏
页码:2667 / 2687
页数:21
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