Open Access
ARTICLE
NUMERICAL SIMULATION OF A DOUBLE SKIN WITH SECONDARY VENTILATION FLOW ON ADIABATIC WALL
M. Bouraouia, M. S. Rouabaha, A. Abidi-Saadb,c,d,*, A. Korichie, C. Popab
, G. Polidorib
a,b Laboratoire de génie climatique, Département de génie climatique, Faculté des Sciences de la Technologie. Université Frères Mentouri –
Constantine 1. Campus Ahmed Hamani, 25000 Constantine, Algeria
b
GRESPI/Thermomécanique, UFR sciences Exactes et Naturelle, Campus du Moulin de la Housse-BP 1039, 51687 Reims, France
c Laboratoire d’Energétique Appliquée et de Pollution, Université Constantine 1, Constantine 25000, Algeria
d Faculté des Hydrocarbures et Energies renouvelables et Sciences de la terre et de l’univers, Université Kasdi Merbah, 30000 Ouargla, Algérie
e
Laboratoire de Mécanique, Physique et Modélisation Mathématique, Université de Médéa, Médéa, Algeria
* Corresponding Author: Email:
Frontiers in Heat and Mass Transfer 2017, 8, 1-6. https://doi.org/10.5098/hmt.8.18
Abstract
Study concerning a double skin flow with secondary ventilation was conducted numerically, in order to understand the basic mechanisms of the free
convection in an open channel asymmetrically heated with uniform heat flux density (510 W/m
2
). The vertical channel corresponds to a double skin
façade, which was immersed in a tank filled with water. The tank corresponds to the environment which allows us to overcome pressure conditions at
the inlet and the outlet of the channel. The use of water allows neglecting radiation effect. The mass conservation equations of momentum and energy
are solved using the finite volume method and numerical simulations are performed using Ansys Fluent CFD software. Our interest, in this work, is
the study of the influence of the position and the size of an opening in the adiabatic wall, which represents secondary ventilation, on the flow
dynamics and the heat transfer.
Keywords
Cite This Article
Bouraoui, M., Rouabah, M. S., Abidi-Saad, A., Korichi, A., Popa, C. (2017). NUMERICAL SIMULATION OF A DOUBLE SKIN WITH SECONDARY VENTILATION FLOW ON ADIABATIC WALL.
Frontiers in Heat and Mass Transfer, 8(1), 1–6.