Premium
Numerical simulation of turbulent impinging jet on a rotating disk
Author(s) -
AbdelFattah A.
Publication year - 2006
Publication title -
international journal for numerical methods in fluids
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.938
H-Index - 112
eISSN - 1097-0363
pISSN - 0271-2091
DOI - 10.1002/fld.1375
Subject(s) - mechanics , turbulence , nozzle , physics , reynolds stress , centrifugal force , jet (fluid) , reynolds number , rotation (mathematics) , shear stress , momentum (technical analysis) , classical mechanics , flow (mathematics) , geometry , mathematics , thermodynamics , finance , economics
The calculations of quasi‐three‐dimensional momentum equations were carried out to study the influence of wall rotation on the characteristics of an impinging jet. The pressure coefficient, the mean velocity distributions and the components of Reynolds stress are calculated. The flow is assumed to be steady, incompressible and turbulent. The finite volume scheme is used to solve the continuity equation, momentum equations and k –ε model equations. The flow characteristics were studied by varying rotation speed ω for 0⩽ω⩽167.6 rad/s, the distance from nozzle to disk ( H / d ) was (3, 5, 8 and 10) and the Reynolds number Re base on V J and d was 1.45 × 10 4 . The results showed that, the radial velocity and turbulence intensity increase by increasing the rotation speed and decrease in the impingement zone as nozzle to disk spacing increases. When the centrifugal force increases, the radial normal stresses and shear stresses increase. The location of maximum radial velocity decreases as the local velocity ratio (α) increases. The pressure coefficient depends on the centrifugal force and it decreases as the distance from nozzle to plate increases. In impingement zone and radial wall jet, the spread of flow increases as the angular velocity decreases The numerical results give good agreement with the experiment data of Minagawa and Obi ( Int. J. of Heat and Fluid Flow 2004; 25 :759–766). Copyright © 2006 John Wiley & Sons, Ltd.