
- •National Aviation University engineering mechanics of liquid and gas
- •Laboratory work 1 determination of reynolds’ critical number Brief theoretical information
- •Work Procedure
- •Laboratory work 2
- •Determination of resistance coefficient
- •And pressure losses along a pipe line
- •Brief theoretical information
- •Work procedure
- •Laboratory work 3 determination of local resistances coefficients Brief theoretical information
- •Work procedure
- •Laboratory work 4 determination of discharge coefficients of liquid flow through orifices and mouthpieces Brief theoretical information
- •1. Discharge coefficients of liquid flow through an orifice in a thin wall.
- •Work procedure
- •2. Discharge coefficients of liquid flow through cylindrical nozzles
- •Work procedure
- •Laboratory work 5
- •Ventury flow meter as an example of engineering application of bernulli ‘s equiation Brief theoretical information
- •Work procedure
- •Laboratory work 6 centrifugal pump testing Brief theoretical information
- •Work procedure
- •Appendix 1
- •Appendix 2
- •Appendix 3
- •Appendix 4
- •Appendix 5
Work procedure
1.Fill in reservoir 1 with water (Fig. 4.2).
2.Open quickly the tank choke and put calibrating tank 3 under the stream.
3.Open faucet for filling tank 1 with water and fix its level as H.
4.Measure H, and coordinates X and Y of some flow points with two rulers. Determine coefficients with formula 4.3
5.Measure time T and volume of water W in the calibrating tank.
6.Determine
actual
,
and theoretical
flow
rates and coefficient
.
7.Determine
flow contraction coefficient by formula
.
8. Calculate resistance coefficient .
9. Put results of measurements and calculations into table 4.1.
10. Compare these results with those given in the manual. Make conclusions.
Table4.1
Pressure head H, cm |
|
|
Ordinate Y, cm |
|
|
Abscissa X, cm |
|
|
Speed Coefficient |
|
|
Time for filling the calibrating tank T, s |
|
|
Measured volume W, cm3 |
|
|
Actual
flow rate
|
|
|
Theoretical
flow rate |
|
|
Rate Coefficient |
|
|
Flow contraction Coefficient |
|
|
Coefficient of resistance |
|
|
2. Discharge coefficients of liquid flow through cylindrical nozzles
Nozzle is a short tube attached to the hole in a thin wall. Cylindrical nozzles are short cylindrical tubes of the length of three - four diameters. Cylindrical nozzles may be of external (Fig. 4.4, a) and internal (Fig. 4.4, b) shape.
The jet, on entering the pipe, is being contracted and then stars expending and fulfilling the pipe.
Fig. 4.4. Scheme of liquid efflux through cylindrical nozzles
In the liquid flow the nozzle forms a contraction section where vacuum occurs. Presence of vacuum is explained by the speed value at the contracted section 1-1 comparing to the speed at the flow outlet (section 2-2), and therefore pressure in the contracted section is less than atmospheric.
At large Pressure Head (H 14 m for water) the flow regime changes suddenly. The flow jet tears away of the wall and flow efflux starts to be of orifice type. The similar phenomena are observed in short mouthpieces when atmospheric pressure bursts into the vacuum zone.
At the first regime of operation the area of flow cross-section (2-2) equals to the area of nozzle cross-section (ε=1) and speed is less in the nozzle than in the orifice because of losses.
Liquid
flow rate through nozzles shows to be greater than that through the
orifices. The nozzle sucks in liquid and makes speed increase. Taking
into account
that for nozzle
=
1, one has
.
The experiments stated, that discharge coefficient for external cylindrical nozzle is = 0,81...0,82.
In internal cylindrical nozzle coefficient gets a lower value because of more difficult entrance conditions and is equal to 0,71. Flow contraction in internal nozzle is greater than in external, therefore changing of flow running shape starts at some lower pressure head H.
Liquid flow rate through mouthpieces is determined by formula 4.6 and liquid speed - by formula 4.1.