
- •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
6. The basic hydrostatic equation
Let us consider the basic case of equilibrium of a fluid when the only body force acting on it is the force of gravity and develop an equation which would enable us to determine the hydrostatic pressure at any point of a given fluid volume. In this case, of course, the free surface of a liquid is a horizontal plane.
Referring to Fig. 6, acting on the free surface of the liquid in the vessel is a pressure p0. Let us determine the hydrostatic pressure p at an arbitrary point M at a depth h from the surface.
Taking an elementary area dS with point M as its centre, erect a vertical cylindrical fluid element of height h and consider the equilibrium conditions for this element. The pressure of the liquid on the base of the cylinder is external with respect to the latter and is normal to the base, i. e., it is directed upward.
Summing the forces acting vertically on the cylinder, we have
pdS —podS —γhdS = 0,
where the last term represents the weight of the liquid in the cylinder. The pressure forces acting on the sides of the cylinder do not enter the equation as they are normal to the side surface. Eliminating dS and transposing,
p = po + hγ. (2.2)
This is the hydrostatic equation with which it is possible to calculate the pressure at any point of a still liquid. The hydrostatic pressure, it will be observed, is composed of the external pressure p0 acting on the boundary surface of the liquid and the pressure exerted by the weight of the overlying layers of the liquid.
The value of p0 is the same for any point of a liquid volume. Therefore, taking into account the second property of hydrostatic pressure, it may be said that a liquid transmits pressure equally in all directions (Pascal's law).
It will be also observed from Eq. (2.2) that pressure in a liquid increases with depth according to a linear law and is the same for all points at a given depth.
*These equations have the form:
Asurface layer where the pressure is the same at all points iscalled
a surface
of equal pressure, or
equipotential
surface. In
the case
considered the equipotential surfaces are horizontal planes, the
free
surface being one of them.
Let us take at an arbitrary elevation a horizontal datum level from which a vertical coordinate z is to be measured. Denoting the coordinate of point M as z and the coordinate of the free surface of the liquid as z0, and substituting z0— z for h in Eq. (2.2), we obtain
But M is an arbitrary point, hence, for the stationary fluid element
The
coordinate z
is
called the
elevation. The
term
,
which is also a
linear quantity, is called the pressure
head, and
the sum
is
called the piezometric
head.
The piezometric head is thus constant for the whole volume of a stationary fluid.
These results can be obtained in more definite form by integrating the differential equilibrium equations for a fluid (see Appendix).