
- •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
3. Forces acting on a fluid. Pressure
In hydraulics, a fluid is treated as a continuum, i. e., a continuous medium filling a portion of space completely, without having any empty spaces. Thereby the molecular structure of matter is neglected and even infinitely small fluid particles are assumed to consist of a great number of molecules.
As a fluid will always yield with time to the slightest stress, it cannot be subject to concentrated forces. Any force acting upon a fluid is distributed uniformly throughout the volume (mass) or along the surface. Accordingly, the external forces acting on any given volume of fluid may be body or surface forces.
Body forces are proportional to the mass or, for homogeneous substances, the volume of the fluid. They arise, first of all, from the force of gravity and the forces produced in a fluid at rest inside an accelerated vessel or flowing in a channel which itself is moving with an acceleration. Body forces also appear as the "effective" D'Alembert forces in developing equations of fluid motion.
Surface forces are distributed continuously over the whole surface of a fluid and, in the case of uniform distribution, are proportional to the surface area. These forces are due to the direct action of all the surrounding fluid on a given volume or to the action of other bodies (solid, liquid or gaseous) in contact with the given fluid. In the most general case, a surface force AjR acting on a given area AS may be directed at an angle to that area and it can be resolved into a normal component AP and a tangential component AT1 (Fig. 1). The former is called the pressure force, the latter is the friction, or shear, force.
Both body and surface forces are usually considered as unit forces, i. e.,they are referred to the corresponding units: body force to a unit mass and surface force to a unit area. As body force equals the product of mass times acceleration, a body force acting on a unit mass is numerically equal to the respective acceleration.
By hydrostatic pressure (often referred to as simply "pressure") is meant the pressure force exerted on a unit area. If the pressure force is uniform over the area, or if the mean value of the hydrostatic pressure is required, the latter is given by the formula
(1.1)
In the most general case the hydrostatic pressure at a point corresponds to the limiting value of the ratio AP/AS as the elementary area AS shrinks to differential value at this point:
(1.2)
If pressure is measured above absolute zero, it is called absolute pressure. If it is measured either above or below atmospheric pressure as a base, it is called gauge pressure. Hence, absolute pressure Pab equals atmospheric, or barometric, pressure patm plus gauge pressure pg:
Fig.
1. Components of a surface force
A unit of pressure commonly used in engineering is the standard atmosphere:
The shear stress, or friction force, in a liquid is denoted by the Greek letter τ (tau) and, like pressure, is given by the limit
(1.3)