Author:
Munas Fathima Rehana,Kok Hwa Yu,Yusoff Norwahida,Muzathik Abdul Majeed,Ismail Mohd Azmi
Abstract
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.
Publisher
Universiti Putra Malaysia
Subject
General Earth and Planetary Sciences,General Environmental Science
Reference63 articles.
1. Al-Khalil, K., Ferguson, T., & Phillips, D. (1997). A hybrid anti-icing ice protection system. In 35th Aerospace Sciences Meeting and Exhibit (p. 302). American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-302
2. Al-Khalil, K. (2007, January). Thermo-mechanical expulsive deicing system-TMEDS. In 45th AIAA Aerospace Sciences Meeting and Exhibit (p. 692). American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-692
3. Asante, C. J., Pokhrel, M., & Cho, J. (2016). CFD simulation study of de-icing on a pitot tube. International Journal of Applied Engineering Research, 11(5), 2986-2989.
4. Azam, Q., Ismail, M. A., Mazlan, N. M., & Bashir, M. (2016). Numerical comparison of drag coefficient between nacelle lip-skin with and without bias acoustic liner. International Review of Mechanical Engineering, 10(6), 390-394. https://doi.org/10.15866/ireme.v10i6.9427
5. Azam, Q., & Ismail, M. A. (2017, August 2). Noise abatement system in commercial aircraft by using Bias Acoustic Liner on nacelle lip-skin. In International Conference on Vibration, Sound and System Dynamics (ICVSSD) (p. 49-54). Universiti Sains Malaysia. https://www.researchgate.net/publication/320584447