Aerodynamic Noise Prediction in Internal Flows Using LES and Linear Euler Equations

Author(s):  
Fabien Crouzet ◽  
Philippe Lafon ◽  
Tobias Buchal ◽  
Dominique Laurence
2017 ◽  
Author(s):  
Rahul Gurav ◽  
Kishor D Udawant ◽  
Ramkumar Rajamanickam ◽  
N V Karanth ◽  
S R Marathe

2006 ◽  
Vol 2006.2 (0) ◽  
pp. 439-440
Author(s):  
Yasushi SHIGENAGA ◽  
Shigehisa FUNABASHI ◽  
Masatoshi WATANABE ◽  
Yoshihiro TAKADA

2011 ◽  
Vol 52-54 ◽  
pp. 1388-1393
Author(s):  
Jun Tao ◽  
Gang Sun ◽  
Ying Hu ◽  
Miao Zhang

In this article, four observation points are selected in the flow field when predicting aerodynamic noise of a multi-element airfoil for both a coarser grid and a finer grid. Numerical simulation of N-S equations is employed to obtain near-field acoustic information, then far-field acoustic information is obtained through acoustic analogy theory combined with FW-H equation. Computation indicates: the codes calculate the flow field in good agreement with the experimental data; The finer the grid is, the more stable the calculated sound pressure level (SPL) is and the more regularly d(SPL)/d(St) varies.


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