- •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
52. Hydraulic losses in pump. Plotting rated characteristic curve
As stated earlier, Htz is the head that would have been developed by a pump if there were no head losses inside it. The actual head Hpump (see Sec. 48) is less than the theoretical head by the total losses inside the pump:
where Σhpump = total head loss in pump (at intake, in impeller and volute).
The ratio of the actual head to the theoretical head for a finite number of vanes is called the hydraulic efficiency, denoted ηh. Thus,
Hydraulic efficiency is always higher than total efficiency as it takes into account only head losses inside the pump. It follows from Eqs (12.18) and (12.21) that
where is given by Eqs (12.7) and (12.12).
The hydraulic losses inside the pump Hpump are conveniently treated as the sum of the following two components.
1. Ordinary hydraulic losses, i.e., losses due to friction and partly to eddy formation inside the pump. As turbulent flow is the common regime in a centrifugal pump, this type of head losses increases approximately as the square of the discharge and can be expressed by the equation
where k{ is a constant depending on the hydraulic efficiency and the dimensions of the pump.
2. Shock losses at impeller and volute entrances. If the relative velocity wx of the fluid at the entrance to a vane passage is tangent to the vane, the fluid is entering the impeller smoothly, without shock or eddy formation. Shock losses in this case are nil. But this is possible only at some definite rated or normal discharge Qo and corresponding radial entrance velocity (vir)o (Fig. 138).
If the actual discharge Q is more or less than the rated discharge Qo and the radial entrance velocity v1r is more or less than (vlr)0 the relative velocity w makes an angle у with the tangent to the vane and the fluid flows past the vane at some positive or negative angle of approach. The effect is that of the fluid impinging on the vane, with eddies forming on the opposite side. Thus, energy is degraded in the impact and eddy formation. The velocity parallelograms for the same peripheral velocities corresponding to these ton-rated operating conditions are shown by broken lines in Fig. 138. One of the parallelograms corresponds to the inequality Q > Qo, the other, to — Q < Qo.
Shock losses can be assumed to vary as the square of the difference between the actual discharge and the discharge when they are zero, i. e.,
Shock losses at the volute entrance are of the same nature as at the impeller intake, the minimum being at about the same rate of discharge Qo, and are included in the quantity h2.
The total loss of head inside the pump is the sum of the two losses considered, i.e.,
The characteristic curves of a pump at uniform rotational speed (n = const) are plotted as follows.
First draw for H as a function of Q atn = const the theoretical characteristic curves for and for a finite number of vanesz. These are inclined straight lines (Fig. 139). Below the Q axis plot the curves for the change in the two components hi and h2 of the head losses in the pump. Summing the ordinates of the two curves gives the curve Σhpump as a function of the discharge. Now, in accordance with Eq. (12.20), subtract Σhpump from Htz which gives the curve Σhpump = =f(Q), i. e., the actual characteristic of the pump for a constant rpm.
The curve H pump = f(Q) in Fig. 139 is typical of a centrifugal pump. The maximum value of the head Hpamp is commonly obtained neither at zero discharge nor at Q= Qo, but at some intermediate value of Q.
Plotting the characteristic curves by the method described is not very accurate in view of the difficulty of determining the coefficients ki and k2 in Eqs (12.22) and (12.23). Therefore the characteristics are commonly plotted by direct experiment, i.e., in testing a pump.
For this a throttling device (some type of valve) is installed atthe outlet pipe of a pump operating at a constant rotational speed. The degree of opening of the valve is gradually changed during a test. For example, at first the valve is wide open. Then the pump is gradually throttled down and the discharge and head are measured. When the valve is completely open, the discharge is maximum and the head is minimum, being equal to the loss of head in the pipeline (point С in Fig. 140). As the valve is throttled, the discharge falls and the head rises to a maximum (point B). As the discharge is further reduced the head also drops somewhat, till at Q = 0 (point A), when the valve is closed completely, the head reaches a value higher than the average but below the maximum.
This is the so-called shutoff head. It will be observed that even complete closure of the valve does not present any danger to thepump or pipeline as no further increase in head develops if the1 number of rpm does not change. For this reason centrifugal pumps, unlike displacement pumps, do not have to be fitted with relief valves.