Drag force on a cylinder in an air tunnel

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SUMMARY

The discussion focuses on calculating the net drag force acting on a cylinder placed in an air tunnel, with air density set at 1.23 kg/m³. The net force was determined using linear momentum balance, resulting in a value of F=95.78 N. The participants highlighted the importance of defining a control volume that adequately captures the mass flow dynamics around the cylinder, particularly the velocity profile behind the cylinder, which varies with the y-coordinate. There was also a consensus that the velocity function provided was incorrect, as it did not accurately reflect the expected behavior of airflow around the cylinder.

PREREQUISITES
  • Understanding of linear momentum balance in fluid dynamics
  • Familiarity with control volume analysis
  • Knowledge of airflow behavior around cylindrical objects
  • Basic principles of drag force calculation
NEXT STEPS
  • Study the principles of control volume analysis in fluid mechanics
  • Learn about the Navier-Stokes equations and their application in airflow problems
  • Investigate the effects of air density on drag force calculations
  • Explore computational fluid dynamics (CFD) tools for simulating airflow around objects
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Students in mechanical engineering, aerospace engineering, and physics, particularly those focusing on fluid dynamics and drag force calculations in airflow scenarios.

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Homework Statement


Let's have a cylinder in air tunnel. The air is flowing around cylinder. I want to calculate a net force acting on the cylinder. Part of the incoming air hits the cylinder and its trajectory direction changes. For that reason we can see straight behind the cylinder lower velocity (29 m/s) that is increasing with y coordinate.
20170512_155645.jpg

The air density is constant 1.23 kg/m3.

Homework Equations


In order to calculate (through the linear momentum bilance) the net force acting on cylinder, I have to consider control volume, that has mass outlet just behind the cylinder (that is above and under cylinder there are no mass flows). For that I need to consider sufficiently big height (Δy) of the control volume. Unfortunately I missed the teacher explanation of how to calculate this. Moreover I don't understand the given v2 function - I'm sure its wrong because at first v2 increases with y to some maximal value and then it convergate back to 30 m/s again - so this v2 function is deffinitely wrong.
Do you have some experience with that type of tasks?

The Attempt at a Solution


Through mass bilance I have to find minimal height of control volume with outlet only behind the cylinder.
Then from control surface dimensions and given velocities I calculate the net force acting on the cylinder.
The correct result is F=95.78 N
 
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What is the exact problem statement? Please copy it instead of describing it. Sometimes details can be important.

The flow velocity has to be larger than the wind tunnel velocity in some parts behind the obstacle, otherwise you would put more air into the tunnel than air goes out.

The region of y considered should be large enough to cover all relevant perturbations of the object I guess.
 
20170514_233639.jpg

20170514_233651.jpg
 
If you are just given the velocity profile in this 2 m meter region, I guess that is all you can use. Looks odd, but if the problem statement wants that...
 

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