
- •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
36. Suppressed contraction. Submerged jet
Suppressed contraction occurs when efflux through an orifice is affected by the proximity of the walls of a reservoir. When the orifice is concentric with the centre line of the reservoir (Fig. 85) the walls tend to guide the liquid approaching the orifice, thus preventing full contraction beyond the orifice. The contraction is less than in efflux from a reservoir of infinite size; the coefficient of contraction increases, and as a consequence, the coefficient of discharge increases as well.
A theoretical investigation of the efflux of an ideal fluid from a flat reservoir of finite height and infinite width through a slot in the end wall was carried out by N. E. Joukowski as far back as 1890.
For a low-viscous liquid flowing through a round orifice in the centre of the end wall of a circular cylindrical reservoir the coefficient of contraction can be found in terms of the contraction coefficient for complete contraction from the following empirical formula:
(9.9)
where
is
the ratio of the orifice area to the cross-sectional area of the
tank.
When
contraction. of the jet is suppressed the loss coefficient ζand
the velocity coefficient φ
can be regarded as being independent of n
(if,
of course, n
is
not too close to unity); for low-viscous fluids the
approximate values are
and
The discharge coefficient is easily found from the relationship
and the rate of discharge is given by the formula
In applying this equation to the case of suppressed contraction it should be remembered that the rated head is the total head
This means that besides the piezometric head the velocity head in the reservoir must also be taken into consideration. As the velocity head is usually unknown, it is desirable to have a formula expressing the rate of discharge for suppressed contraction not in terms of the total head H but in terms of the piezometric head.
Such a formula is easily obtained from Bernoulli's equation and the continuity equation written between sections 1-1 and 2-2 (see Fig. 85):
From this
and
(9.10)
where
(9.11)
If an orifice is close to a side wall of a tank the contraction is suppressed over a part of the perimeter of the jet as shown in Fig. 86. In this case, too, the contraction and discharge coefficients ε2 and ε2 are greater than for unsuppressed contraction.
The coefficient μ2 can be found from the empirical formula
(9.12)
where ζ = form coefficient, equal to 0.128 for circular and 0.152 for square orifices;
П = perimeter of orifice;
ΔП = fraction of the perimeter adjoining the wall.
Many engineering problems are concerned with discharge of a liquid below the surface of the same liquid in another vessel (Fig. 87). This is known as a submerged jet.
The total kinetic energy of the jet is dissipated in eddy formation, as in the case of an abrupt expansion. The Bernoulli equation between sections 7-7 and 3-3 (where the velocities can be assumed zero) takes the form
or
where H = rated head;
v = velocity at the vena contracta;
ξ = loss coefficient of the orifice, which is approximately the same as in the case of a free jet.
Hence,
and
Thus, the equations are the same as for a free jot, only in the present case the head H is the difference between the piezoraetric heads on both sides of the wall.
The coefficients of contraction and discharge of a submerged jet can be assumed the same as of a free jet.