On the computation of low-subsonic turbulent pipe flow noise with a hybrid LES/LPCE method

  • Hwang, Seungtae
  • Moon, Young J.
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초록

Aeroacoustic computation of a fully-developed turbulent pipe flow at Rer. 175 and M = 0.1 is conducted by LES/LPCE hybrid method. The generation and propagation of acoustic waves are computed by solving the linearized perturbed compressible equations (LPCE), with acoustic source DP(x,t)/Dt attained by the incompressible large eddy simulation (LES). The computed acoustic power spectral density is closely compared with the wall shear-stress dipole source of a turbulent channel flow at Re,= 175. A constant decaying rate of the acoustic power spectrum, f(-8/5) is found to be related to the turbulent bursts of the correlated longitudinal structures such as hairpin vortex and their merged structures (or hairpin packets). The power spectra of the streamwise velocity fluctuations across the turbulent boundary layer indicate that the most intensive noise at omega(+) < 0.1 is produced in the buffer layer with fluctuations of the longitudinal structures (k(z)R < 1.5).

키워드

Low-subsonicTurbulent pipe flow noiseComputational aeroacousticsTurbulent burstsBOUNDARY-LAYERMACH NUMBERPRESSURE FLUCTUATIONSAEROACOUSTICSRADIATIONSPECTRUMSOUND
제목
On the computation of low-subsonic turbulent pipe flow noise with a hybrid LES/LPCE method
저자
Hwang, SeungtaeMoon, Young J.
DOI
10.5139/IJASS.2017.18.1.48
발행일
2017-03
유형
Article
저널명
International Journal of Aeronautical and Space Sciences
18
1
페이지
48 ~ 55