Appendix C Useful Theoretical Approaches and Formulas
493
Therefore, the stream function 1/J (x, y) finally takes the form:
1/J ( x, y) = Va (y cos () - x sin ()) ,
(C.67)
and the streamlines are given by equations:
Va (y cos () - x sin ()) = K n ,
(C.68)
in which Kn is the constant. The subscript n indicates a value of constant K,
corresponding to the nth streamline. If we rewrite Eq. (C.68) in another form:
Kn
y = tan(} x +
,
Va cos ()
(C.69)
we find that streamlines are straight lines of slope tan (), as should be expected.
Consider now the flow through cross-section A-B in Fig. C.4. The discharge
of flow through this cross-section is:
(C.70)
Assuming that a difference between two adjacent streamlines is constant and
equal to 11K, the discharge for any two adjacent streamlines becomes:
I1Q = Kn - K n- 1 = 11K.
(C.7l)
In a similar way it can be found that the velocity potential function, 1>,
corresponding to the uniform flow shown in Fig. C.4, is:
1> (x, y) = Va (x cos () + y sin ()),
(C.72)
and at equipotential lines where the velocity potential, 1>, is constant, we have:
Va(x cos () + y sin (}) = Pn ,
(C.73)
where Pn is the constant corresponding to the nth equipotential line.
Let us rewrite Eq. (C.73) as:
1
Pn
y = - - - x + - - .
tan ()
Va sin ()
(C.74)
Thus, equipotential lines are also straight lines but of slope (-l/tan ()). Comparing this slope to the slope of the streamline (Eq. C.69), we find that equipotential lines are perpendicular to the streamlines as their slopes are negative
reciprocals.
493
Therefore, the stream function 1/J (x, y) finally takes the form:
1/J ( x, y) = Va (y cos () - x sin ()) ,
(C.67)
and the streamlines are given by equations:
Va (y cos () - x sin ()) = K n ,
(C.68)
in which Kn is the constant. The subscript n indicates a value of constant K,
corresponding to the nth streamline. If we rewrite Eq. (C.68) in another form:
Kn
y = tan(} x +
,
Va cos ()
(C.69)
we find that streamlines are straight lines of slope tan (), as should be expected.
Consider now the flow through cross-section A-B in Fig. C.4. The discharge
of flow through this cross-section is:
(C.70)
Assuming that a difference between two adjacent streamlines is constant and
equal to 11K, the discharge for any two adjacent streamlines becomes:
I1Q = Kn - K n- 1 = 11K.
(C.7l)
In a similar way it can be found that the velocity potential function, 1>,
corresponding to the uniform flow shown in Fig. C.4, is:
1> (x, y) = Va (x cos () + y sin ()),
(C.72)
and at equipotential lines where the velocity potential, 1>, is constant, we have:
Va(x cos () + y sin (}) = Pn ,
(C.73)
where Pn is the constant corresponding to the nth equipotential line.
Let us rewrite Eq. (C.73) as:
1
Pn
y = - - - x + - - .
tan ()
Va sin ()
(C.74)
Thus, equipotential lines are also straight lines but of slope (-l/tan ()). Comparing this slope to the slope of the streamline (Eq. C.69), we find that equipotential lines are perpendicular to the streamlines as their slopes are negative
reciprocals.
