Heat transfer through tube walls can be promoted using a ribbed tube configuration. Most of the ribs used in previous reports have equal height along the tube length. In this numerical study, we investigate the heat transfer and pressure drop in a transverse ribbed tube where ribs of unequal heights are mounted such that the tops of the ribs form a zigzag shape. Four configurations were studied. Each configuration had a set of two neighboring ribs of different heights. The set was repeated along the tube length to form a zigzag shape. The rib height ratios, e2/e1, of the four sets were 0.25, 0.5, 0.75, and 1.0. The ratios of the height of the taller rib, pitch, and width to the tube diameter were kept constant at values of e1/d = 0.1, p/d =...
An experimental work on heat transfer enhancement in a round tube by insertion of double twisted tap...
AbstractAn experimental work on heat transfer enhancement in a round tube by insertion of double twi...
In the fast development of advanced gas turbines with increasing output power, the inlet temperature...
Numerical investigation have been performed by solving the conservation equations of mass, momentum,...
The thermal and hydraulic performance of rib-roughened, dimpled and offset strip fin tubes has been ...
This paper presents a three-dimensional numerical investigation carried out in turbulent forced con-...
A numerical study was undertaken for investigating the heat transfer enhancement in a tube with tria...
The thermal performance was examined computationally for the stationary channels with rib turbulator...
The present study employs square cross-section ribbed channels with different arrangements of downst...
The heat transfer and pressure loss characteristics on a square channel with two opposite surfaces ...
Square cross-section ribbed channels with deflectors are computationally simulated to determine thei...
In the quest for enhancing heat-transfer for the internal cooling channels of advanced turbo-machine...
An experimental investigation of heat transfer in a rectangular channel with angled rib turbulators,...
Numerical investigation have been performed by solving the conservation equations of mass, momentum,...
This paper is an investigation of the heat transfer augmentation in the fully-developed portion of a...
An experimental work on heat transfer enhancement in a round tube by insertion of double twisted tap...
AbstractAn experimental work on heat transfer enhancement in a round tube by insertion of double twi...
In the fast development of advanced gas turbines with increasing output power, the inlet temperature...
Numerical investigation have been performed by solving the conservation equations of mass, momentum,...
The thermal and hydraulic performance of rib-roughened, dimpled and offset strip fin tubes has been ...
This paper presents a three-dimensional numerical investigation carried out in turbulent forced con-...
A numerical study was undertaken for investigating the heat transfer enhancement in a tube with tria...
The thermal performance was examined computationally for the stationary channels with rib turbulator...
The present study employs square cross-section ribbed channels with different arrangements of downst...
The heat transfer and pressure loss characteristics on a square channel with two opposite surfaces ...
Square cross-section ribbed channels with deflectors are computationally simulated to determine thei...
In the quest for enhancing heat-transfer for the internal cooling channels of advanced turbo-machine...
An experimental investigation of heat transfer in a rectangular channel with angled rib turbulators,...
Numerical investigation have been performed by solving the conservation equations of mass, momentum,...
This paper is an investigation of the heat transfer augmentation in the fully-developed portion of a...
An experimental work on heat transfer enhancement in a round tube by insertion of double twisted tap...
AbstractAn experimental work on heat transfer enhancement in a round tube by insertion of double twi...
In the fast development of advanced gas turbines with increasing output power, the inlet temperature...