作者: R. Marcondes Orselli , B. Souza Carmo , R. Lauterjung Queiroz
DOI: 10.1007/S40430-018-0982-2
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摘要: The purpose is to simulate numerically the flow and noise on Advanced Noise Control Fan (ANCF). ANCF model was developed by NASA Glenn Research Center provide measurement data of a turbofan its corresponding generated noise. aim numerical simulations predict accurately tonal as well broadband content ducted rotor/stator using reference provided far-field measurements.