2. If an incompressible laminar flow (through pipe area A₁) is forced through a narrow orifice, it will be focused into a smaller area, known as the vena contracta (with cross-sectional area A₂), as shown below: Orifice area Ao A₁ P₁ Flanges Pipe wall P2 Vena con- tracta area A₂ Eddies Intense turbulence and loss of energy Pressure tappings Reestablished flow pattern Figure 3: Flow through an orifice. The orifice focuses the laminar flow to a vena contracta, increasing its velocity. Beyond the orifice, the flow becomes turbulent for some distance until a laminar flow pattern is re-established. By measuring pres- sures upstream (p₁) and downstream (p2) from the orifice, the vol- umetric flow rate (Q) can be determined. (a) If the velocity of the fluid entering the pipe is u₁, what is the velocity u₂ at the end of the vena contracta? (b) What is the velocity of the fluid after the flow pattern has been reestablised? (c) What is the relationship between pressure drop (p₁ - p2) and volumetric flow rate Q?

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
icon
Related questions
Question

Need the solution by the end of the day! Thank you!

2. If an incompressible laminar flow (through pipe area \(A_1\)) is forced through a narrow orifice, it will be focused into a smaller area, known as the *vena contracta* (with cross-sectional area \(A_2\)), as shown below:

![Diagram](attachment) 

**Figure 3: Flow through an orifice.** The orifice focuses the laminar flow to a *vena contracta*, increasing its velocity.

Beyond the orifice, the flow becomes turbulent for some distance until a laminar flow pattern is re-established. By measuring pressures upstream (\(p_1\)) and downstream (\(p_2\)) from the orifice, the volumetric flow rate (\(Q\)) can be determined.

(a) If the velocity of the fluid entering the pipe is \(u_1\), what is the velocity \(u_2\) at the end of the *vena contracta*?

(b) What is the velocity of the fluid after the flow pattern has been reestablished?

(c) What is the relationship between pressure drop (\(p_1 - p_2\)) and volumetric flow rate \(Q\)?

---

**Explanation of Diagram:**

The diagram illustrates an orifice in a pipe with different sections labeled:

- **Orifice area \(A_0\)**: The initial area of the pipe before the orifice.
- **Flanges**: Segments around the orifice.
- **Vena contracta area \(A_2\)**: The smaller area where the flow converges, resulting in increased velocity.
- **Intense turbulence and loss of energy**: Turbulent flow occurs immediately after the *vena contracta*.
- **Reestablished flow pattern**: The flow returns to a laminar state further downstream.
- **Pressure tappings**: Areas where pressures \(p_1\) and \(p_2\) are measured.
- **Eddies**: Circular flow patterns indicating turbulence.

The flow is initially laminar, becomes turbulent through the orifice, and eventually returns to a laminar state.
Transcribed Image Text:2. If an incompressible laminar flow (through pipe area \(A_1\)) is forced through a narrow orifice, it will be focused into a smaller area, known as the *vena contracta* (with cross-sectional area \(A_2\)), as shown below: ![Diagram](attachment) **Figure 3: Flow through an orifice.** The orifice focuses the laminar flow to a *vena contracta*, increasing its velocity. Beyond the orifice, the flow becomes turbulent for some distance until a laminar flow pattern is re-established. By measuring pressures upstream (\(p_1\)) and downstream (\(p_2\)) from the orifice, the volumetric flow rate (\(Q\)) can be determined. (a) If the velocity of the fluid entering the pipe is \(u_1\), what is the velocity \(u_2\) at the end of the *vena contracta*? (b) What is the velocity of the fluid after the flow pattern has been reestablished? (c) What is the relationship between pressure drop (\(p_1 - p_2\)) and volumetric flow rate \(Q\)? --- **Explanation of Diagram:** The diagram illustrates an orifice in a pipe with different sections labeled: - **Orifice area \(A_0\)**: The initial area of the pipe before the orifice. - **Flanges**: Segments around the orifice. - **Vena contracta area \(A_2\)**: The smaller area where the flow converges, resulting in increased velocity. - **Intense turbulence and loss of energy**: Turbulent flow occurs immediately after the *vena contracta*. - **Reestablished flow pattern**: The flow returns to a laminar state further downstream. - **Pressure tappings**: Areas where pressures \(p_1\) and \(p_2\) are measured. - **Eddies**: Circular flow patterns indicating turbulence. The flow is initially laminar, becomes turbulent through the orifice, and eventually returns to a laminar state.
Expert Solution
trending now

Trending now

This is a popular solution!

steps

Step by step

Solved in 4 steps with 4 images

Blurred answer
Knowledge Booster
Fluid Dynamics
Learn more about
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, mechanical-engineering and related others by exploring similar questions and additional content below.
Similar questions
Recommended textbooks for you
Elements Of Electromagnetics
Elements Of Electromagnetics
Mechanical Engineering
ISBN:
9780190698614
Author:
Sadiku, Matthew N. O.
Publisher:
Oxford University Press
Mechanics of Materials (10th Edition)
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:
9780134319650
Author:
Russell C. Hibbeler
Publisher:
PEARSON
Thermodynamics: An Engineering Approach
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:
9781259822674
Author:
Yunus A. Cengel Dr., Michael A. Boles
Publisher:
McGraw-Hill Education
Control Systems Engineering
Control Systems Engineering
Mechanical Engineering
ISBN:
9781118170519
Author:
Norman S. Nise
Publisher:
WILEY
Mechanics of Materials (MindTap Course List)
Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:
9781337093347
Author:
Barry J. Goodno, James M. Gere
Publisher:
Cengage Learning
Engineering Mechanics: Statics
Engineering Mechanics: Statics
Mechanical Engineering
ISBN:
9781118807330
Author:
James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:
WILEY