
- •Chapter I introduction
- •1. The subject of hydraulics
- •2. Historical background
- •3. Forces acting on a fluid. Pressure
- •4. Properties of liquids
- •Chapter II hydrostatics.
- •5. Hydrostatic pressure
- •6. The basic hydrostatic equation
- •7. Pressure head. Vacuum. Pressure measurement
- •8. Fluid pressure on a plane surface
- •Fig. 12. Pressure distribution on a rectangular wall
- •9. Fluid pressure on cylindrical and spherical surfaces. Buoyancy and floatation
- •Fig. 18. Automatic relief valve.
- •Relative rest of a liquid
- •10. Basic concepts
- •11. Liquid in a vessel moving with uniform acceleration in a straight line
- •12. Liquid in a uniformly rotating vessel
- •The basic equations of hydraulics
- •13. Fundamental concepts
- •14. Rate of discharge. Equation of continuity
- •15. Bernoulli's equation for a stream tube of an ideal liquid
- •16. Bernoulli's equation for real flow
- •17. Mead losses (general considerations)
- •18. Examples of application of bernoulli's equation to engineering problems
- •Chapter V flow through pipes. Hydrodynamic similarity
- •19. Flow through pipes
- •20. Hydrodynamic similarity
- •21. Cavitati0n
- •Chapter VI laminar flow
- •22.Laminar flow in circular pipes
- •23. Entrance conditions in laminar flow. The α coefficient
- •24. Laminar flow between parallel boundaries
- •Chapter VII turbulent flow
- •25. Turbulent flow in smooth pipes
- •26. Turbulent flow in rough pipes
- •27. Turbulent flow in noncircular pipes
- •Chapter VIII local features and minor losses
- •28. General considerations concerning local features in pipes
- •29. Abrupt expansion
- •30. Gradual expansion
- •31. Pipe contraction
- •32. Pipe bends
- •33. Local disturbances in laminar flow
- •34. Local features in aircraft hydraulic systems
- •Chapter IX flow through orifices, tubes and nozzles
- •35. Sharp-edged orifice in thin wall
- •36. Suppressed contraction. Submerged jet
- •37. Flow through tubes and nozzles
- •38. Discharge with varying head (emptying of vessels)
- •39. Injectors
- •Relative motion and unsteady pipe flow
- •40. Bernoulli's equation for relative motion
- •41. Unsteady flow through pipes
- •42. Water hammer in pipes
- •Chapter XI calculation of pipelines
- •43. Plain pipeline
- •44. Siphon
- •45. Compound pipes in series and in parallel
- •46. Calculation of branching and composite pipelines
- •47. Pipeline with pump
- •Chapter XII centrifugal pumps
- •48. General concepts
- •49. The basic equation for centrifugal pumps
- •50. Characteristics of ideal pump. Degree of reaction
- •51. Impeller with finite number of vanes
- •52. Hydraulic losses in pump. Plotting rated characteristic curve
- •53. Pump efficiency
- •54. Similarity formulas
- •55. Specific speed and its relation to impeller geometry
- •56. Relation between specific speed and efficiency
- •57. Cavitation conditions for centrifugal pumps (according to s.S. Rudnev)
- •58. Calculation of volute casing
- •59. Selection of pump type. Special features of centrifugal pumps used in aeronautical and rocket engineering
44. Siphon
A siphon is a plain gravity pipeline some portion of which lies higher than the feeding reservoir (Fig. 115). Flow is caused by the elevation head #, the liquid first rising to a height Ht above the free surface with atmospheric pressure and then flowing down the height H2.
Characteristic of a siphon is that the pressure in the whole of the ascending section and part of the descending section is less than atmospheric.
For a liquid to start flowing through a siphon the latter must first be filled completely. If the siphon is a small hose it can be filled by immersing into a reservoir or evacuating the air from the lower end. If the siphon is a stationary metal pipeline it must be provided with a valve at the summit to evacuate the air. The air can be evacuated by a displacement pump (see further on) or an air ejector (Sec. 18).
Write
Bernoulli's equation between sections0-0
and
2-2
(Fig.
115), where the velocities are assumed to be zero and the pressure
is atmospheric.
This gives
or
Thus, the rate of discharge through a siphon is determined by the difference of the elevations H and the resistance of the pipeline and does not depend on the height of the summit Ht. This, however, is true only within certain limits. With Ht increasing, the absolute pressure px at the summit (section 1-1) drops. When it becomes equal to the vapour pressure cavitation begins and the discharge decreases. Vapour collects at the bend, forming so-called vapour locks, and the flow stops.
Accordingly, in designing siphons precautions must be taken to prevent the pressure pi at the summit from falling too low. If the rate of discharge and all the dimensions of the siphon are known, the absolute pressure pt can be found from Bernoulli's equation taken between sections 0-0 and 1-1:
If the minimum permissible pressure pi and the rate of discharge are known, the maximum elevation H, can be computed from the equation.
45. Compound pipes in series and in parallel
Consider several pipes of different length and diameter and with \ different local features joined in series (Fig. 116).
It is evident that the rate of discharge through all portions of the compound pipes is the same and the total loss of head between points
M and N is the sum of the head losses in each of them. Thus, the basic equations are:
These equations define the rule for plotting the characteristics of a compound series of pipes.
Suppose that we are given (or have plotted ourselves) the characteristics of the three pipes in Fig. 117. To plot the curve for the series from M to N, we must, in accordance with Eq. (11.5), compound the head losses for equal rates of discharge, i. е., sum the ordinates of all three curves at equal abscissas.
In
the most general case the velocities at the beginningM
and
end N
of the
pipeline are different and the expression for the required head
for the whole pipeline M-N
must
contain, unlike Eq. (11.1), the
difference between the velocity heads
at the end and the beginning,
i. e.,
Now consider several pipes joined in parallel between points M and N (Fig. 118). For simplicity's sake we shall assume them to be all in the horizontal plane.
Notation: pressure at M and N = pM and р„ respectively; rate of discharge through main (i. e., before and after the loop) = Q; rates of discharge through the parallel pipes = Q1 Q2 and Q3 respectively; total head losses in the parallel pipes = Σhv Σh2 and Σh3 respectively.
First write down the obvious equation:
From this we draw the important conclusion that
i.e., the head losses in parallel pipes are equal.
These losses can be expressed in terms of the respective rates ot discharge in general form as follows:
where the coefficients к and the exponents m are found, depending on the flow regime, from Eq. (11.2) or (11.3).
Consequently, besides Eq. (11.7), we have from Eq. (11.8) two more equations:
Equations (11.7), (11.9), (11.10) can be employed to solve such a typical problem as determination of the rates of discharge Qv Q2, Q3 in parallel pipes if the rate of discharge Q of the main and the pipe dimensions are known.
Applying Eq. (11.7) and the rule (11.8) we can develop as many equations as there are parallel pipes between two points M and N.
In
calculating aircraft fuel systems a common problem is: Giventotal
discharge and the lengths of parallel pipes, to determine the
diameters necessary to ensure a specified rate of discharge through
each
of them. The solution of such a problem is presented in
an
example
at the end of the chapter.
The following important rule follows from the relationships in (11.7) and (11.8): in order to plot the characteristics of compound pipes in parallel it is necessary to sum the abscissas (rates of discharge) of the respective curves at equal ordinates (heads). An example of such a construction is presented in Fig.119.
Obviously, the relationships and rules for compound pipes in parallel hold good for the case of pipes 1, 2, 3, etc. (see Fig. 118), not converging at one point N but delivering the liquid at different points with equal pressures and with equal elevation heads at the end sections. If the latter condition is not observed, the pipes cannot be regarded as parallel and should be considered under the heading of the branching pipe problem in the following section.