Effect of chevron nozzle penetration on aero-acoustic characteristics of jet at M = 0.8
Author:
Publisher
IOP Publishing
Subject
Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanical Engineering
Link
https://iopscience.iop.org/article/10.1088/1873-7005/aa8501/pdf
Reference56 articles.
1. An evaluation of various concepts of reducing supersonic jet noise
2. An experimental study of subsonic jet noise and comparison with theory
3. Aeroacoustics of a Mach 0.9 Jet with Chevron-Microjet Combination
4. The effect of streamwise vortices on the aeroacoustics of a Mach 0.9 jet
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1. Numerical Investigation on the Effect of Geometric Parameters of Chevron Nozzle on Generation of Steamwise Vortices in High Subsonic Jets;Journal of Aerospace Sciences and Technologies;2023-07-29
2. Acoustic Modeling of Compressible Jet from Chevron Nozzle: A Comparison of URANS, LES and DES Models;Symmetry;2022-09-21
3. Jet noise sources for chevron nozzles in under-expanded condition;International Journal of Aeroacoustics;2022-06-21
4. Correlation analysis of flow and sound in non-isothermal subsonic jets based on large eddy simulations;Physics of Fluids;2022-04
5. A Wavelet-Based Time-Frequency Analysis on the Supersonic Jet Noise Features with Chevrons;Fluids;2022-03-16
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