- •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
8. Fluid pressure on a plane surface
The total pressure on a plane surface inclined at an arbitrary angle a to the horizontal (Fig. 11) can be determined with the help of the hydrostatic equation (2.2). For this calculate the pressure P of the fluid on any portion of the surface of arbitrary outline of area S. The x axis is directed along the line of intersection of the plane with the free surface, and the у axis is perpendicular to that line in the given plane.
The elementary pressure on a differential area dS is
where p0 = pressure on the free surface;
h = depth of the area dS.
To determine the total pressure P, integrate over the whole
area S:
where у = distance of the centre of the area dS from the x axis.
The quantity ,it will be recalled from the course in
mechanics, is the moment of the area S about the axis Ox and is equal to the product of the area and the distance yc of its centre of gravity from that axis. Hence,
whence
where hc = depth of submersion of the centre of gravity; and finally
(2.6)
i. e., the total pressure of a liquid on a plane area is equal to the product of the area and the static pressure at its centre of gravity.
If the pressure p0 is atmospheric, the gauge pressure of the liquid on a plane surface is
(2.6)`
The centre of pressure, which is the point of application of the resultant force on the area, is found as follows.
As the external pressure p0 is transmitted equally to all points of the area £, its resultant is applied at the centre of gravity of the area. The location of the point of application of the resultant gauge pressure (point D) is found from the well-known equation of mechanics which states that the moment of a resultant about an axis Ox is equal to the sum of the moments of the component forces about that axis, i.e.,
,
where yD = distance of the point of application of force Pg from the x axis.
Expressing Pg and dPg in terms of yc and у to determine yDi we have
where moment of inertia of the area S about the axis Ox.
Taking into account that
where -moment of inertia of the area S about its own centre line parallel to Ox, we finally obtain
(2.7)
Thus, the point of application of force Pg is located below the centre of gravity of the area at a distance
If p0 is equal to atmospheric pressure and if it acts on both sides I of the surface, point D will be the centre of pressure. If p0 is greater I than atmospheric pressure, the centre of pressure is found according I to the laws of mechanics as the point of application of the resultant p of forces Pg and p0 S. The greater the latter force as compared with I the former the closer, apparently, is the centre of pressure to the • centre of gravity of the area S.
Fig. 12. Pressure distribution on a rectangular wall
To determine the second coordinate xD of the centre of pressure, the moment equation should be written with respect to the у axis.
In the special case when the surface is a rectangle with one side in the free surface of the liquid the centre of pressure is located very simply. As the pressure diagram for the forces acting on a submerged surface represents a right-angled triangle (Fig. 12) whose centre of gravity is located at 1/3 the altitude b of the triangle, the centre of pressure will also be located at 1/3 6 from the lower edge of the rectangle.
In engineering we often have to deal with the pressure of fluids on plane surfaces, e.g., against pistons in various hydraulic machines and devices (see examples and Chapter XIV). In these cases the pressure p0 is usually so great that the centre of pressure may be assumed to coincide with the centre of gravity of the area on which it is acting.