- •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
46. Calculation of branching and composite pipelines
We shall call a branching pipeline one in which several pipes have a common cross-section where the flows diverge or converge. Such pipelines are common in aircraft fuel systems (main and refuelling), hydraulic transmissions and ground fuel supply systems at aerodromes.
Let a main branch at M-M (Fig. 120) into three pipes of different size and with different local features and let the elevation heads zv z2, z3 at the end sections and the pressures pv p2 p3 also be different. We shall investigate the relation between the pressure pM at section M-M and the rates of discharge Ql Q2 Q3 through the respective pipes when the direction of flow is as indicated by the arrows in the drawing.*
As in the case of parallel pipes,
Bernoulli's equation between section M-M and the end section of, say, the first pipe yields (neglecting the difference in velocity head)
Denoting the sum of the first two members in the right-hand side of the equation Д>у z\ and expressing the last, as before, in terms of the discharge, we obtain
♦ In aircraft systems reversal of the flow is prevented by nonreturn valves.
Similarly, for theother two pipes
We thus have four equations with four unknown quantities: Q1, Q2, Q3 and pM. A graphical solution is more convenient. For this, construct a curve for each pipe by plotting as a function of Q according to the above equations and then compound them in the same way as in the case of parallel pipes, i.e., sum the abscissas Q for equal ordinates (Fig. 121). The resulting stepped curve characterises the whole of the branching pipeline and makes it possible to determine the rates of discharge from the pressure pM and vice versa.
If the flow is reversed, i. e., from the several sections 1, 2, 3 to the section M-M (see Fig.120), the signs of the head losses are reversed and, consequently, the curves are plotted downwards.
A composite pipeline is one which consists of compound pipes in series and branching or parallel pipes. Composite pipelines, both with gravity flow and with pumps, are usually calculated by the graphoanalytical method, i. e., by using characteristic curves.
To calculate and plot the characteristics of a composite pipeline it is broken down into a number of plain pipelines, the calculations and curve constructions for which are carried out as described before. The characteristics of the parallel or branching pipes are compounded as described in Sec. 45, then the characteristics of the parallel or branching pipes are added to the characteristics of the series according to the equations (11.5).
In this way it is possible to plot the characteristics of any composite pipeline for both turbulent and laminar flow.
Examples on the plotting of composite pipeline characteristics are given at the end of the chapter.