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Experimental investigation of the acoustic pressure in cavity of a two-dimensional sonic crystal

✍ Scribed by Liang-Yu Wu; Lien-Wen Chen; Chia-Ming Liu


Publisher
Elsevier Science
Year
2009
Tongue
English
Weight
527 KB
Volume
404
Category
Article
ISSN
0921-4526

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An experiment was conducted on a two-dimensional bifurcated, supersonic inlet to investigate the aeroacoustics at take-o! and landing conditions. A 104)1 mm (4)1 in) diameter turbofan simulator was coupled to the inlet to generate the noise typical of a turbofan engine. Aerodynamic and acoustic data