Modern Control Engineering

(Chris Devlin) #1
102 Chapter 4 / Mathematical Modeling of Fluid Systems and Thermal Systems

where steady-state liquid flow rate, m^3 sec


coefficient, m^2 sec


steady-state head, m


For laminar flow, the resistance Rlis obtained as


The laminar-flow resistance is constant and is analogous to the electrical resistance.


If the flow through the restriction is turbulent, the steady-state flow rate is given by


(4–1)


where steady-state liquid flow rate, m^3 sec


coefficient, m2.5sec


steady-state head, m


The resistance Rtfor turbulent flow is obtained from


Since from Equation (4–1) we obtain


we have


Thus,


The value of the turbulent-flow resistance Rtdepends on the flow rate and the head. The


value of Rt, however, may be considered constant if the changes in head and flow rate


are small.


By use of the turbulent-flow resistance, the relationship between QandHcan be


given by


Such linearization is valid, provided that changes in the head and flow rate from their


respective steady-state values are small.


In many practical cases, the value of the coefficient Kin Equation (4–1), which depends


on the flow coefficient and the area of restriction, is not known. Then the resistance may


be determined by plotting the head-versus-flow-rate curve based on experimental data


and measuring the slope of the curve at the operating condition. An example of such a plot


is shown in Figure 4–1(b). In the figure, point Pis the steady-state operating point. The tan-


gent line to the curve at point Pintersects the ordinate at point Thus, the slope


of this tangent line is Since the resistance Rtat the operating point Pis given by


2H the resistance Rtis the slope of the curve at the operating point.



Q



,


2H



Q



.


A0,-H



B.


Q=


2H


Rt


Rt=


2H


Q


dH


dQ


=


21 H


K


=


21 H 1 H


Q


=


2H


Q


dQ=


K


21 H


dH


Rt=


dH


dQ


H=


K=


Q=


Q=K 1 H


Rl=


dH


dQ


=


H


Q


H =


K =


Q =


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