Solution to transient Navier-Stokes equations by the coupling of differential quadrature time integration scheme with dual reciprocity boundary element method

2009 ◽  
Vol 59 (2) ◽  
pp. 215-234 ◽  
Author(s):  
C. Bozkaya ◽  
M. Tezer-Sezgin
2007 ◽  
Author(s):  
Jure Ravnik ◽  
Leopold Škerget ◽  
Zoran Žunič ◽  
Theodore E. Simos ◽  
George Psihoyios ◽  
...  

2017 ◽  
Vol 25 (04) ◽  
pp. 1750006 ◽  
Author(s):  
V. Cutanda Henríquez ◽  
P. Risby Andersen ◽  
J. Søndergaard Jensen ◽  
P. Møller Juhl ◽  
J. Sánchez-Dehesa

In recent years, boundary element method (BEM) and finite element method (FEM) implementations of acoustics in fluids with viscous and thermal losses have been developed. They are based on the linearized Navier–Stokes equations with no flow. In this paper, such models with acoustic losses are applied to an acoustic metamaterial. Metamaterials are structures formed by smaller, usually periodic, units showing remarkable physical properties when observed as a whole. Acoustic losses are relevant in metamaterials in the millimeter scale. In addition, their geometry is intricate and challenging for numerical implementation. The results are compared with existing measurements.


2016 ◽  
Vol 2016 ◽  
pp. 1-13 ◽  
Author(s):  
M. Nouroozi ◽  
M. Pasandidehfard ◽  
M. H. Djavareshkian

A fixed-length Boundary Element Method (BEM) is used to investigate the super- and partial cavitating flows around various axisymmetric bodies using simple and reentrant jet models at the closure zone of cavity. Also, a simple algorithm is proposed to model the quasi-3D cavitating flows over elliptical-head bodies using the axisymmetric method. Cavity and reentrant jet lengths are the inputs of the problem and the cavity shape and cavitation number are some of the outputs of this simulation. A numerical modeling based on Navier-Stokes equations using commercial CFD code (Fluent) is performed to evaluate the BEM results (in 2D and 3D cases). The cavitation properties approximated by the present research study (especially with the reentrant jet model) are very close to the results of other experimental and numerical solutions. The need for a very short time (only a few minutes) to reach the desirable convergence and relatively good accuracy are the main advantages of this method.


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