Aeroacoustic Investigation of Passive and Active Control on Cavity Flowfields Using Delayed Detached Eddy Simulation

Author:

Liu Yu1ORCID,Shi Yong12,Tong Mingbo2ORCID,Zhao Fei1,Chen Binqi3ORCID

Affiliation:

1. Institute of Manned Space System Engineering, Beijing 100094, China

2. College of Aerospace and Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

3. School of Aeronautics and Astronautics, University of Electronic Science and Technology of China, Chengdu 611731, China

Abstract

In the present study, CFD simulation with delayed detached eddy simulation (DDES) is performed to investigate an open cavity at Mach 0.85. A clean cavity and cavity with passive and active control methods, including sawtooth spoiler, flat-top spoiler, crossflow rod, and steady leading edge blowing, are analyzed. The results obtained from all the control methods are compared with clean cavity, and all the flow control methods show positive effect on the overall sound pressure level reduction with the decrement up to 8 dB. The effect of active control on sound pressure level in the cavity is much better than that of passive control, with the magnitude of tone noise decreasing by 20-30 dB. The main focus of this investigation is to test the noise suppression effect by passive and active control methods.

Funder

Fundamental Research Funds for the Central Universities

Publisher

Hindawi Limited

Subject

Aerospace Engineering

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