Achieving cylindrical duct modes generation in spinning mode synthesizer via a least-square identification of the global calibration factor

Author:

Huang Shichun,Pan Xingjian,Yu Liang,Jiang Weikang

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Acoustics and Ultrasonics

Reference29 articles.

1. Current engine noise and reduction technology;Nesbitt;CEAS Aeronautical J,2019

2. Aircraft noise generation and assessment: executive summary;Bertsch;CEAS Aeronautical J,2019

3. Design and development of the spinning mode synthesizer;Seiner;National Aeronautics and Space Administration,1973

4. Perulli M, Ville J. Measurement of absorbing materials acoustic parameters in the working conditions of intake duct. 4th Aeroacoustics Conference. 1977: 1332.

5. Ville J M. Experimental investigation of the radiation of sound from an unflanged duct and a bellmouth, including the flow effect. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980.

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