Published November 2004 | Version v1
Journal article

Buoyancy effects laminar slot jet impinging on a surface with constant heat flux

Description

The two-dimensional laminar air jet issuing from a nozzle of half which terminates at height above a flat plate normal to the jet is numerically on the flow and thermal structure of the region near impingement. The impinging surface is maintained at a constant heat flux condition. The full Navier-Stocks and energy equations are solved by a finite difference method to evaluate the velocity profiles and temperature distribution. The governing parameters and their ranges are: Reynolds number Re, 10-50, Grashof number Gr, 0-50, Richardson number Ri=Gr/ Re2, Non dimensional nozzle height H,2-3. Results of the free streamline, local friction factor and heat transfer coefficient are graphically presented. It is found that enhancement of the heat transfer rate is substantial for high Richardson number conditions. Although the laminar jet impingement for isothermal condition has been already studied, however the constant heat flux has not been studied enough. the present paper will analyze a low velocity air jet, Which can be used for cooling of a simulated electronics package

Availability note (English)

Available from Atomic Energy Organization of Iran

Additional details

Additional titles

Original title (Persian)
Motale-e tasir-e niroo'ha-ye shenavari bar zarib enteqal hararat dar barkhord jet aram be safh-e ba shar hararat-ye sabet

Publishing Information

Journal Title
Journal of Faculty of Engineering, Tehran University
Journal Volume
38
Journal Issue
no.1
Journal Page Range
p. 513-523
ISSN
1026-0803

INIS

Country of Publication
Iran, Islamic Republic of
Country of Input or Organization
Iran, Islamic Republic of
INIS RN
36011838
Subject category
S42: ENGINEERING;
Resource subtype / Literary indicator
Numerical Data
Descriptors DEI
BUOYS; COOLING; HEAT FLUX; HEAT TRANSFER; JETS; NUMERICAL DATA; SURFACES; TEMPERATURE DISTRIBUTION
Descriptors DEC
DATA; ENERGY TRANSFER; INFORMATION