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Effect of nozzle rotation angles and sizes on thermal characteristic of swirl anti-icing t /Mohd Azmi Ismail , Jian Wang

Effect of nozzle rotation angles and sizes on thermal characteristic of swirl anti-icing t/Mohd Azmi Ismail a nd Jian Wang

Abstract The Federal Aviation Administration requires all ai rcraft manufacturers to ad here to maximum noise level standards. Thus, a bias acoustic l i ner is introduced. to intensi fy the noise eq u ipment system. as well as preven t ice accumulation on the nacelle 0-chamber. The hotspot phenomenon. by the Piccolo tu be anti-i<.:ing sysh:m. cou ld damage t he bias acoustic liner. Therefore. a swi rl ant i-icing system is fu rther i n vestigated, to reduce t he hotspot t:ffcct on the bi as acoustic l iner. The pr

Contributor(s): Mohd Azmi Ismail - Author Jian Wang - Author Language: English Subject Keywords: aircraft ; hotspot ; anti-icing First presented to the public: 5/18/2018 Original Publication Date: 3/3/2020 Previously Published By: Universiti Sains Malaysia Place Of Publication: School of Mechanical Engineering Citation: Extents: Number of Pages - 9 License Grantor / Date Granted:   / ( View License ) Date Deposited 2020-03-03 10:28:26.416 Submitter: Nor Hayati Ismail

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