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Erschienen in:

2020 | OriginalPaper | Buchkapitel

Review of Hot Air Anti-icing System Inside Bias Acoustic Liner

verfasst von : Lee Chern Khai, Mohd Azmi Ismail, Yu Kok Hwa, Khairil Faizi bin Mustafa, Nurul Musfirah Mazlan, Pravinth Balthazar

Erschienen in: Proceedings of International Conference of Aerospace and Mechanical Engineering 2019

Verlag: Springer Singapore

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Abstract

Ice accumulation and noise dissipation in aircraft nacelle lip–skin are the two main issues faced by the aviation industry nowadays. In order to prevent ice formation and reduce engine noise at the same time, hot air anti-icing system has been incorporated into bias acoustic liner. This paper discusses briefly the introduction on aircraft crashes that happen due to icing issues, literature review on the types of hot air anti-icing systems and acoustic liners used today and its application in computational fluid dynamics as well as a summary on the advantages of bias acoustic liner in nacelle lip–skin.

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Vorheriges Kapitel The Effect of Flow Control on Wing-In-Ground Craft Hull-Fuselage for Improved Aerodynamics Performance

Nächstes Kapitel Physical and Mechanical Characterization of Kenaf Fiber Filament Wound Composite Produced Using Vacuum-Bagging and Heat-Shrink Tube Method

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Titel: Review of Hot Air Anti-icing System Inside Bias Acoustic Liner
verfasst von: Lee Chern Khai
Mohd Azmi Ismail
Yu Kok Hwa
Khairil Faizi bin Mustafa
Nurul Musfirah Mazlan
Pravinth Balthazar
Verlag: Springer Singapore
Buch: Proceedings of International Conference of Aerospace and Mechanical Engineering 2019
Print ISBN: 978-981-15-4755-3

Electronic ISBN: 978-981-15-4756-0

Copyright-Jahr: 2020
DOI: https://doi.org/10.1007/978-981-15-4756-0_45

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