
- •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
The basic equations of hydraulics
13. Fundamental concepts
We shall commence our study of liquids in motion with an examination of so-called ideal-fluid flow. An ideal fluid is an imaginary fluid whose viscosity is zero. As in real motionless fluids, the only strains possible in a nonviscous fluid are normal compressive strains; i.e., pressure forces.
Pressure forces in a flowing ideal fluid possess the same properties as in a motionless fluid, i. e., on the boundary they are directed along the inward normal; at any point inside the fluid they are the same in all directions.*
Flow may be steady or unsteady.
In steady flow the flow characteristics at a fixed position in space do not change with time; pressure and velocity change only with the change of position of a fluid particle. Mathematically this can be expressed as follows:
;
;
;
;
where the velocity subscripts denote the respective projections on a set of cartesian axes.
In the general case of unsteady flow, pressure and velocity vary with both position and time, i. e.,
Unsteady
flow is observed when A liquid pours under gravity out
of a sink in the bottom of a vessel and in the suction, and
pressure pipes of an ordinary reciprocating piston pump.
Steady flow is observed when a liquid is flowing out of a vessel
in which a constant level is maintained or in a looped pipeline
through which a liquid is driven by a centrifugal pump with a
uniform speed of rotation.
Ivestigation of steady flow is much simpler than of unsteady flow. In this book we shall consider mainly steady flow, only touching on some special cases of unsteady flow.
In steady flow the fluid particles travel along pathlines which do not change with time.
In unsteady flow different particles passing through a given point in space will be moving along different pathlines. Accordingly, to investigate the flow pattern for every given moment of time the concept of streamline is introduced.
A streamline is a line in a flowing fluid the tangent to which at any point shows the direction of the velocity vector of the fluid particles at that point (Fig. 23). In steady flow, evidently, streamlines and pathlines coincide and do not change with time.
A stream tube is a tubular space bounded by a surface consisting of streamlines (Fig. 24). When the cross-section of a stream tube is contracted to zero, a streamline is obtained in the limit.
The velocity vectors at all points of the surface of a stream tube are tangential to the surface. There being no normal components of the velocity, no particle of the liquid can enter or leave the stream tube, except at the ends. Thus, a stream tube can be regarded as surrounded by impenetrable walls and therefore treated as an elementary stream.
At first we shall imagine streams of finite size as being made up of bundies of elementary stream tubes. Due to differences in velocity the stream tubes slip with respect to one another, but there is no mixing.
* The latteris proved in the samp way as for a motionlees fluid (see Sec 5) the equations of motion are developed for an elementary tetrahedron, taking into account the D’Aiembert inertia forces Whiehy together with the body forces, tend to zero when the tetrahedron is contracted to a point.
A cross-section of a stream is, generally, a surface passed through the stream normal to the streamlines. We shall usually be considering portions of streams in which the streamlines are parallel and, therefore, the cross-sections are plane.