Consider steady, incompressible, laminar flow of a Newtonian fluid in an infinitely lons round pipe annulus of inner radius R i and outer radius R 0 (Fig. 9-98). Ignore the effects of gravity. A constant negative pressure gradient ∂ P / ∂ x is applied in the x -direction, ( ∂ P / d x ) = ( P 2 − P 1 ) / ( x 2 − x 1 ) , where x 1 and x 2 are two arbitrary locations along FIGURE P9-98 the x -axis, and P 1 and P 2 are the pressures at those two locations. The pressure gradient may be caused by a pump and/or gravity. Note that we adopt a modified cylindrical coordinate system here with x, instead of z for the axial component, namenly, ( r , θ , x ) and ( u r , u θ , u ) . Derive an expression for the velocity field in the annular space in the pipe.
Consider steady, incompressible, laminar flow of a Newtonian fluid in an infinitely lons round pipe annulus of inner radius R i and outer radius R 0 (Fig. 9-98). Ignore the effects of gravity. A constant negative pressure gradient ∂ P / ∂ x is applied in the x -direction, ( ∂ P / d x ) = ( P 2 − P 1 ) / ( x 2 − x 1 ) , where x 1 and x 2 are two arbitrary locations along FIGURE P9-98 the x -axis, and P 1 and P 2 are the pressures at those two locations. The pressure gradient may be caused by a pump and/or gravity. Note that we adopt a modified cylindrical coordinate system here with x, instead of z for the axial component, namenly, ( r , θ , x ) and ( u r , u θ , u ) . Derive an expression for the velocity field in the annular space in the pipe.
Solution Summary: The author explains the derivation for expression for the velocity field in the annular space in pipe.
Consider steady, incompressible, laminar flow of a Newtonian fluid in an infinitely lons round pipe annulus of inner radius
R
i
and outer radius
R
0
(Fig. 9-98). Ignore the effects of gravity. A constant negative pressure gradient
∂
P
/
∂
x
is applied in the x-direction,
(
∂
P
/
d
x
)
=
(
P
2
−
P
1
)
/
(
x
2
−
x
1
)
, where
x
1
and
x
2
are two arbitrary locations along
FIGURE P9-98 the x-axis, and
P
1
and
P
2
are the pressures at those two locations. The pressure gradient may be caused by a pump and/or gravity. Note that we adopt a modified cylindrical coordinate system here with x, instead of z for the axial component, namenly,
(
r
,
θ
,
x
)
and
(
u
r
,
u
θ
,
u
)
. Derive an expression for the velocity field in the annular space in the pipe.
4-105. Replace the force system acting on the beam by an equivalent resultant force and couple
moment at point B.
A
30 in.
4 in.
12 in.
16 in.
B
30%
3 in.
10 in.
250 lb
260 lb
13
5
12
300 lb
Sketch and Describe a hatch coaming and show how the hatch coamings are framed in to ships strucure?
Sketch and describe hatch coamings. Describe structrual requirements to deck plating to compensate discontinuity for corners of a hatch. Show what is done to the deck plating when the decks are cut away and include the supporting members.
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