Exploratory and Numerical Examination of Blending of Four …
25
5 Governing Equations
Head (h)
H = y ×
S hg /S air
− 1
( 1 )
where
y
difference in manometer reading
S hg specific gravity of mercury
S air specific gravity of air.
Velocity (V )
V =
√
2gH
(2)
where
g acceleration due to gravity in m/s
2
H head.
6 Results and Discussions
In spite of various results obtained, the contour representation displays the effects
predominantly. So, contours of velocity magnitude and velocity vector, numerical
and graphical illustrations for various pitch circle diameter while jets diameter d j
= 10 mm and at inlet velocity V i = 315 m/s have been provided in the following
sections.
EFFEC From Figs. 3, 4 and 5, unmistakably the impact of pitch circle dia (PCD) is
ruling over the forms of speed size. Following a similar pattern, the impact of PCD is
progressively prevailing close to the divider locale of fly plate and delivering consolidation focuses and joined focuses at short separations for expanding the estimations
of PCD.
Figures 6, 7 and 8 demonstrate the speed vector for various PCDs. The union
focuses and joined focuses can be seen clearly for expanding estimations of pitch
circle dia (PCD).
6.1 Graphical Illustrations
Speed extents for various PCDs when width of planes d j = 10 mm are acquired
numerically and they are outlined graphically through Figs. 9, 10 and 11. It is
25
5 Governing Equations
Head (h)
H = y ×
S hg /S air
− 1
( 1 )
where
y
difference in manometer reading
S hg specific gravity of mercury
S air specific gravity of air.
Velocity (V )
V =
√
2gH
(2)
where
g acceleration due to gravity in m/s
2
H head.
6 Results and Discussions
In spite of various results obtained, the contour representation displays the effects
predominantly. So, contours of velocity magnitude and velocity vector, numerical
and graphical illustrations for various pitch circle diameter while jets diameter d j
= 10 mm and at inlet velocity V i = 315 m/s have been provided in the following
sections.
EFFEC From Figs. 3, 4 and 5, unmistakably the impact of pitch circle dia (PCD) is
ruling over the forms of speed size. Following a similar pattern, the impact of PCD is
progressively prevailing close to the divider locale of fly plate and delivering consolidation focuses and joined focuses at short separations for expanding the estimations
of PCD.
Figures 6, 7 and 8 demonstrate the speed vector for various PCDs. The union
focuses and joined focuses can be seen clearly for expanding estimations of pitch
circle dia (PCD).
6.1 Graphical Illustrations
Speed extents for various PCDs when width of planes d j = 10 mm are acquired
numerically and they are outlined graphically through Figs. 9, 10 and 11. It is