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Numerical Simulation of Wall-Pressure Fluctuations Due to a Turbulent Boundary Layer
Author(s) -
Niloufar Mahmoudnejad,
Klaus Hoffmann
Publication year - 2012
Publication title -
journal of aircraft
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.64
H-Index - 94
eISSN - 1533-3868
pISSN - 0021-8669
DOI - 10.2514/1.c031858
Subject(s) - boundary layer , mechanics , turbulence , computer simulation , direct numerical simulation , flow separation , adverse pressure gradient , materials science , physics , reynolds number
Click on the DOI link to access the article (may not be free.)In this investigation, wall-pressure fluctuations due to a turbulent boundary layer are estimated by various numerical methods. Four different turbulence models, including one- and two-equation models and a recently developed direct numerical simulation scheme, are employed to calculate the pressure and velocity fluctuations. Numerical results are compared with each other as well as with several empirical/semi-empirical mean-square-pressure models and single-point wall-pressure spectrum models. Among all investigated turbulence models, the delayed detached-eddy simulation based on Spalart-Allmaras (DDES-SA) model provided the most-accurate results in association with slope prediction in low-frequency range. Moreover, computation time of the DDES-SA model was shorter than other turbulence models. Comparison of the solutions of the proposed direct numerical simulation scheme and the DDES-SA model shows that the direct numerical simulation scheme provided more-accurate results, especially in the low-frequency region

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