32th Congress of the International Council of the Aeronautical Sciences

04.1 - Material Issues, Fatigue and Damage Tolerance

THE NOISE REDUCTION STUDY OF COMPOSITE ACOUSTIC LINER ON HIGH BYPASS RATIO TURBOFAN AEROENGINE

P. Hou¹, X.-J. Shang¹, Y. Dong¹; ¹Shenyang Aero Engine Research Institute, China

Based on the structure/process integration design and engineering application, this paper provided products of composite acoustic liner for aeroengine. Under the condition of low cost, acoustic tests were carried out by plate specimens, which built platform and data support for aircraft in low noise design.


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