Interaction between periodic disturbances and a turbulent jet


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Abstract

The results of a numerical and experimental investigation of the interaction between harmonic disturbances and a turbulent jet are presented. On the basis of large eddy simulation it is established that the narrow-band noise of a supersonic jet considerably increases, when the forcing amplitude amounts to thousandths and more of the total pressure of the flow within the nozzle. An analysis of the results of a laboratory experiment on the measurement of the longitudinal velocity spectra in the core of a low-velocity jet shows that the acoustic disturbances generated by a fan inside the nozzle lead to the generation of intense tonal hydrodynamic disturbances in the low-velocity jet.

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About the authors

S. A. Cheprasov

Baranov Central Institute of Aviation Motors (CIAM)

Author for correspondence.
Email: cheprasov@ciam.ru
Russian Federation, ul. Aviamotornaya 2, Moscow, 111116

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