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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2023, Vol. 44 ›› Issue (7): 127122-127122.doi: 10.7527/S1000-6893.2022.27122

• Fluid Mechanics and Flight Mechanics • Previous Articles     Next Articles

Simulation and analysis of noise reduction in high⁃temperature and high⁃speed rocket jet by water injection

Junlin LIU1,2, Xihai XU3(), Zhicheng ZHANG2, Xiaoqian CHEN1   

  1. 1.College of Aerospace Science and Engineering,National University of Defense Technology,Changsha  410073,China
    2.Beijing Special Engineering Design and Research Institute,Beijing  100028,China
    3.Research Institute of Aero?Engine,Beihang University,Beijing  100191,China
  • Received:2022-03-08 Revised:2022-03-21 Accepted:2022-05-12 Online:2023-04-15 Published:2022-05-19
  • Contact: Xihai XU E-mail:xuxihai@buaa.edu.cn
  • Supported by:
    National Level Project(ZRHT2020T05);National Natural Science Foundation of China(91952302);National Science and Technology Major Project(J2019-II-0006-0026)

Abstract:

Based on Computational Fluid Dynamics (CFD) and the Mixture multiphase flow model, this study conducts numerical calculation of the average flow field under the conditions of an isolated rocket jet and water injection noise reduction. The influence of water flow on the average temperature, pressure, velocity and turbulent kinetic energy field of the rocket jet under the condition of water injection is analyzed. Reynolds Averaged Navier-Stokes(RANS) based jet noise prediction method is used to predict the spectrum and directivity of turbulent mixing noise and broadband shock noise from the jet with and without water injection. The effect of water injection on the turbulent mixing noise and broadband shock noise of the rocket gas jet at different frequencies and different observation positions is studied, providing a technical basis for the subsequent design of the rocket take-off noise reduction scheme.

Key words: rockets, jet noise, noise reduction by water injection, aeroacoustics, multiphase flow

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