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user's manual for corhyd: an internal diffuser hydraulics model - IfH

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2<br />

2<br />

2<br />

2<br />

Vup<br />

ρ V<br />

V<br />

e<br />

⋅<br />

ρe<br />

⋅<br />

down<br />

up ρe<br />

⋅ Vdown<br />

ζ<br />

e,orig<br />

⋅ ⋅ = ζ<br />

2<br />

e,orig<br />

⋅ = ζ<br />

e<br />

⋅<br />

(5)<br />

V 2<br />

2<br />

2<br />

down<br />

A similar modification is implemented <strong>for</strong> additional entered local losses: If the loss relates to<br />

<strong>an</strong>other reference velocity th<strong>an</strong> the one found in the segment described by the given diameter<br />

2 2<br />

of the Port (D p ), the coefficient is multiplied by the ratio of the two velocities V ,<br />

where<br />

V p<br />

V add<br />

add<br />

V p<br />

is the needed (related) reference velocity <strong>for</strong> the given local loss coefficient <strong>an</strong>d<br />

the velocity due to the given port diameter. However, when entering the loss coefficients,<br />

the user usually does not know the discharge through the port <strong>an</strong>d, there<strong>for</strong>e, does not know<br />

the velocity either. But the discharge through one port does not ch<strong>an</strong>ge when reaching a<br />

different segment of this port. There<strong>for</strong>e, instead of velocities, the modification c<strong>an</strong> be done<br />

regarding the flow devided by the areas:<br />

2<br />

⎛qi<br />

⎞<br />

2<br />

2<br />

V<br />

⎜ A ⎟<br />

add<br />

A<br />

add<br />

p<br />

ζ add = ζ add , orig ⋅ = ζ<br />

2 add , orig ⋅<br />

⎝ ⎠<br />

= ζ<br />

2 add , orig ⋅<br />

(6)<br />

2<br />

V<br />

p<br />

⎛q<br />

A<br />

i<br />

⎞<br />

add<br />

⎜<br />

A<br />

⎟<br />

⎝ p ⎠<br />

where ζ is the original local loss coefficient <strong>an</strong>d is the related area. If there are<br />

add , orig<br />

several known additional local losses, each ζ<br />

add ,i<br />

is determined separately, modified if<br />

necessary <strong>an</strong>d then the sum of all losses is entered into the designated space. Using this<br />

method, very complicated port-riser configurations c<strong>an</strong> be calculated with the program.<br />

A add<br />

2.4.2 Friction losses<br />

Continuous pressure losses due to friction along the walls or boundary layers in a pipeline are<br />

calculated as:<br />

p l = L ρ ⋅ 2<br />

2<br />

e<br />

V<br />

λ ⋅ ⋅ or as headloss p l /γ e = L V<br />

λ ⋅ ⋅<br />

(7)<br />

D 2<br />

D 2g<br />

where λ is the friction coefficient, L the length of the considered pipe section, D the diameter,<br />

V the velocity in the pipe section, <strong>an</strong>d ρ e the density of the effluent. For the calculation of the<br />

friction coefficient λ, the explicit <strong>for</strong>m described by Swamee <strong>an</strong>d Jain (1976) is used:<br />

0.25<br />

(8)<br />

λ =<br />

2<br />

⎡ ⎛ k 5.74 ⎞⎤<br />

⎢lg⎜<br />

s<br />

+<br />

0.9<br />

⎟<br />

3.7 Re<br />

⎥<br />

⎣ ⎝ D ⎠⎦<br />

It is valid <strong>for</strong> −6<br />

k −2<br />

10 < s<br />

3<br />

5<br />

< 10 <strong>an</strong>d 4 ⋅10<br />

< Re < 10 , where ks st<strong>an</strong>ds <strong>for</strong> the equivalent s<strong>an</strong>d<br />

D<br />

roughness <strong>an</strong>d the Reynolds number Re = VD/ν e , where ν st<strong>an</strong>ds <strong>for</strong> the kinematic viscosity<br />

of the effluent.<br />

Values of k s <strong>for</strong> different pipe materials <strong>an</strong>d surface conditions of use are listed in Table 3,<br />

which is <strong>an</strong> excerpt of Idelchik (1986). If only M<strong>an</strong>nings n values are known a conversion to<br />

k s c<strong>an</strong> be done by using the <strong>for</strong>mula:<br />

k s = (n 5.87 (2g)^0.5 ) 6 (9)<br />

Institut für Hydromech<strong>an</strong>ik, Universität Karlsruhe 19

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