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This is the full problem presented by the professor/text book. There is no given

ID: 2075024 • Letter: T

Question

This is the full problem presented by the professor/text book. There is no given Velocity information. I have found a similar Chegg solution, but one that does not account for the minor losses through the nozzle. I'm assuming the approach would be near identical. My question is: would the losses include Kentrance, Knozzle, and Kexit? The problem gives Kentrance and Knozzle. My confusion comes from the linked solution, where they use K=1 for exit. Is this a proper assumption? I didn't see it stated in the linked question statement.

Linked Chegg solution: https://www.chegg.com/homework-help/laboratory-experiment-air-20-c-flows-large-tank-2-cm-diamete-chapter-6-problem-149p-solution-9781259165924-exc

2. In a laboratory experiment, air ( = 1.2 kg/m3, = 0.000015 kg/ms) flows from a very large air tank through a 2 cm diameter smooth pipe open to atmosphere as shown. The flow is metered by a long-radius nozzle of 1 cm diameter, using oil (SG 0.827). The pipe is 8 m long. Following measurements were taken at different flow rates Tank Pressure Pg (Pa) 60 320 120020502470 3500 4900 Manometer Reading h (mm) 638 160295 380 575 820 Friction factor f Volume Flow rate m3hr (theory) Volume Flow rate m3/hr (measured) (a) For each data point, compute the volume flow rate (m3/hr) using the energy equation and pipe flow analysis. Assume a smooth pipe. Consider major and minor losses. Assume minor loss coefficients for entrance (Kentrance 0.5) and nozzle Knozze0.7). Enter friction factor f and volume flow rate values (theory) in the above table. Either use Moody's chart (or the Colebrook relation, this might be better as several data points are given) (b) Compute the volume flow rate (m3/hr) using the measured manometer reading across the nozzle (you will have to first relate the manometer reading and area change across nozzle to the velocity through the nozzle throat and then obtain the flow rate). Enter this value in the above table as well (c) Plot (using Matlab or other software), flow rate versus the flow Reynolds number (Re). Use he solid line for the flow rate obtained from the pipe flow analysis and square symbols for t flow rate obtained from the manometer reading. Both should be plotted on the same figure with proper legend given. Show all steps and attach your program or procedure used to solve this part

Explanation / Answer

I am just answering your doubt and not doing the full numerical.

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So basically there are 5 types of minor losses in a pipe flow.

1. Losses at pipe entrance or exit

2. Losses due to sudden expansion or contraction

3. Losses due to gradual expansion or contraction

4. Losses due to pipe fittings

In the given question, only 1st and 2nd types of losses are occurring.

2nd type of loss occur due to the presence of nozzle which will be compensated by considering K(nozzle)

Also the loss at entrance can be considered by taking K (entrance)

Now the K values for losses at exit are generally taken as 1. This is because when the flow takes place from a pipe to a much larger body of same velocity then its velocity is completely reduced to zero and its kinetic energy is dissipated. Hence the losses are of only one velocity head irrespective of the exit geometry.

Hence your assumption is correct.

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