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This workbook is provided "as is", without warranty of any kind, express or
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Copyright © 2011 Harlan H. Bengtson. All Rights Reserved.
Copyright © 2011 Harlan H. Bengtson. All Rights Reserved.
Tab .
Tab . Contents (current tab)
Contents (current tab)
Tab !.
Tab !. Head oss!"rictional #ressure $rop
Head oss!"rictional #ressure $rop
Tab .
Tab . #ipe "low %ate
#ipe "low %ate
Tab #.
Tab #. %e&uired $iameter
%e&uired $iameter
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#ipe "low!"riction "actor Calculations +: (/.0. units)
for given flow rate, 1, pipe diam., $, pipe length, ,
2 in 3.4333 3.3334 ft 3.35627 533 ft 3.5628 3.233 cfs 8.5 5.69 53,4;4 3.33337;8
(Calculate f with the transition region e&uation and see if differs from the one calculated above.)
*ransition %egion "riction "actor, f: 3.3775
%epeat calc of f using new value of f: 3.3773
Calculation of Head oss, h
, and "rictional #ressure $rop,
∆
#
f,
pipe roughness,
ε
, and fluid properties,
ρ
<
µ
.
$nstructions
:Enter values in blue boxes. Spreadsheet calculates values in yellow bo
.
%etermine &riction &actor, f, assuming completely turbulent flow 'f ( ).# * ! log
+%-$nputs
(enter values in the blue boes)
Calculations
(done by spreadsheet
#ipe $iameter,
%
in = #ipe $iameter,%
=#ipe %oughness, = "riction "actor,
f
=#ipe ength,
0
= Cross-0ect.>rea,1
=#ipe "low %ate,
2
= >ve.?elocity,3
="luid $ensity, slugs!ft8 %eynolds number,
4e
="luid ?iscosity, = lb-sec!ft7
!.
Check on whether the given flow is "completely turbulent flow"f ( '!5log
+)
f
=f
=ε
! =-%6-.76*!.8-4e5f
-!669/
!%epeat again if necessary: 3.3773 3.29 ft "rictional #ressure 93 psf "rictional #ressure 3.7 psi
Copyright © 2010 Harlan H. Bengtson. All Rights Reserved.
f
=.
Calculate h0and :f , using the final value for f calculated in step !;<uations= h
0( f0-%63
!-!g6 and :
f
(
gh
0"rictional Head oss,
h
0 =$rop,
:
f =@oody "riction "actor &uations
ft
#ipe %oughness ?alues
ft!sec
es
/
ft7
#ipe "low!"riction "actor Calculations ++: (/.0. units)
Calculations
9 in 3.8888 3.3334 ft 3.375;3 93 ft 3.3;8 3.6 ft 3.8 5.69 6.4 3.33337;8 774,768(Calculate f with the transition region e&uation and see if differs from the one calculated above.)
*ransition %egion "riction "actor, f: 3.377;
%epeat calc of f using new value of f: 3.377;
%epeat again if necessary: 3.377;
Calculation of "luid "low %ate, 1, for given frictional head loss, h
, pipe
diam., $, pipe length, , pipe roughness,
ε
, and fluid properties,
ρ
<
µ
.
$nstructions
:Enter values in blue boxes. Spreadsheet calculates values in yellow boxes
.
%etermine &riction &actor, f, assuming completely turbulent flow 'f ( ).# * ! log
+%-$nputs
(enter values in the blue boes)
#ipe $iameter,
%
in = #ipe $iameter,%
=#ipe %oughness, = "riction "actor,
f
=#ipe ength,
0
= Cross-0ect.>rea,1
=>llowable Head oss,
h
0 = >ssumed "low %ate,2
="luid $ensity, slugs!ft8 >ve. ?elocity,
3
="luid ?iscosity, = lb-sec!ft7 %eynolds number,
4e
=!.
Check on whether the given flow is "completely turbulent flow"f ( '!5log
+)
f
=f
=f
=ε
! =-%6-.76*!.8-4e5f
-!669/
!9.2 ft!sec
3.93 cfs
AB*: *his is an iterative calculation, because an assumed value of 1 is used to start the
calculations. +f the final calculated value of 1 is different from the assumed value, then the
assumed value of 1 should be replaced with the calculated value of 1, leading to a new
calculated value for 1. *his should be repeated as many times as necessary to get the
calculated value for 1 to be the same as the assumed value. *his iteration typically converges
rather rapidly.
*his spreadsheet shows only the final assumed and calculated values of 1 (when they are e&u
+f the initial assumed value of 1 was 5.4 cfs, then subse&uent calculated and assumed values
for 1, leading to the final solution are as follows:
>ssumed 1, cfs
Calculated 1, cfs
5.4
3.4
3.4
3.8
3.8
3.8
Copyright © 2010 Harlan H. Bengtson. All Rights Reserved.
.
Calculate 3 and 2, using the final value for f calculated in step ! in the %arcy Weisbach e<uatio)3 ( !g5%5h
0-f506
-!9 and 2 ( 3 %
!-#6
"luid ?elocity,
3
=@oody "riction "actor &uations
ft
cfs
#ipe %oughness ?alues
ft!sec ft7
l).
#ipe "low!"riction "actor Calculations +++: ( /.0. units )
Calculation of pipe diameter, $, for given flow rate, 1, pipe length, ,
(AB*: *his is an iterative calculation. >n initial assumed value of $ will be used.)
$nputs
Calculations
73 ft 9 in 3.3334 ft 3.8888 ft 533 ft 3.375;3 3.233 cfs 3.3;8 5.69 2.6 ft!sec 3.33337; 529,2;7(Calculate f with the transition region e&uation and see if differs from the one calculated above.)
*ransistion %egion "riction "actor, f: 3.3783
%epeat calc of f using new value of f: 3.3783
pipe roughness,
ε
, head loss, h
, and fluid properties,
ρ
<
µ
.
$nstructions
:Enter values in blue boxes. Spreadsheet calculates values in yellow boxes
.
%etermine &riction &actor, f, assuming completely turbulent flow 'f ( ).# * ! log
+%- >llowable Head oss,
h
0 = >ssumed #ipe $iam,%
in =#ipe %oughness, = #ipe $iameter,
%
=#ipe ength,
0
= "riction"actor,f
=#ipe "low %ate,
2
= Cross-0ect.>rea,1
= ft7"luid $ensity, slugs!ft8 >ve. ?elocity,
3
="luid ?iscosity, = lb-sec!ft7 %eynolds number,
4e
=!.
Check on whether the given flow is "completely turbulent flow") f ( '!5log
+)
f
=f
=ε
!/
=-%6-.76*!.8-4e5f
-!669/
!9
%epeat again if necessary: 3.3783
3.394 ft = 5.3 in
AB*: *his iterative procedure doesnDt converge smoothly to a solution. +f the calculated pipe diameter in this step is larger than the assumed pipe diameter above, then replace the assumed pipe diameter value with the net larger standard pipe siEe. %epeat until you find the smallest standard pipe diameter that gives a smaller calculated re&uired pipe diameter. *hat is your solution.
'ith the eample values given here, an assumed pipe diameter of 8 inches gives a calculated pipe diameter re&uirement of 8.9 inches, increasing the assumed pipe diameter to the net standard pipe siEe ( 8.4 inches ) gives a calculated pipe diameter re&uirement of 5. inches, so a 8.4 inch siEe is the
minimum standard pipe diameter that will do the Fob.
0tandard nominal /.0. pipe siEes in inches:
5!, 5!9, 8!, 5!7, 8!9, 5, 5 5!9, 5 5!7, 7, 7 5!7, 8, 8 5!7, 9, 4, 2, , 53, 57, 59, 52, 5, 73, 79, 83, 97, 9, 49, 23
Copyright © 2010 Harlan H. Bengtson. All Rights Reserved.