What Is the Angle of the Jet Before Deflection in Aerodynamics?

AI Thread Summary
The discussion revolves around calculating the angle of a jet before deflection in a physics problem involving a sphere suspended under a jet of air. The sphere weighs 20N and the jet has a velocity of 20 m/s and a cross-sectional area of 0.25 m². The participant is uncertain about how to apply trigonometry to find the angle α and questions the validity of their approach, particularly regarding the force calculation of 120N. It is emphasized that the jet is not brought to a complete stop but is only deflected, which affects the calculation of the change in velocity (Δv). A vector diagram is suggested to clarify the relationship between the forces and momentum in the control volume.
Poppietje
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Hello!
This is probably a rather simple problem, but I've been a bit confused about how to approach it. Any kick in the right direction for problem b) would be much appreciated! (Below is the full problem statement and sub-questions also for those who want to practice their physics. The question that I need help with is in bold.)

Homework Statement


xae86.png

A sphere with a weight W = 20N "hangs" under a free homogeneous jet of air. The jet is deflected by the sphere, the original angle α changes to the horizontal. The velocity of the jet before deflection V1 = 20 m/s, the cross-sectional area before deflection A1 = 0.25m2. The air density ρ = 1.2 kg/m3.
Viscous forces on the sphere are neglected.

a) Choose a control volume and draw a vector diagram showing the relationship between the force on the jet and the momentum per second entering and leaving the control volume.
b) Calculate the angle α of the jet before deflection.
Calculate c) V2 and d) A2 of the jet after deflection.

Homework Equations


At this point, all of our problems are to be solved using Bernoulli's equation, the Continuity equation and the Momentum equation. (Though I figure that the angle part is just pure trigonometry. :) )

The Attempt at a Solution


For problem b):
My instinct would be to just take the tan-1 of the values opp./adj., as taught by trigonometry. Problem is, I have no idea how to define these values. I did calculate that the force of the flow at the inlet area is 120N assuming that the flow travels horizontally, giving us what could be used as the value for the adjacent side. I'm just not convinced of if this is the correct approach for solving for α, and even if it was, I'm not sure how to proceed with this information.

Any help would be greatly appreciated! Thank you!
 
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Poppietje said:
Hello!
This is probably a rather simple problem, but I've been a bit confused about how to approach it. Any kick in the right direction for problem b) would be much appreciated! (Below is the full problem statement and sub-questions also for those who want to practice their physics. The question that I need help with is in bold.)

Homework Statement


xae86.png

A sphere with a weight W = 20N "hangs" under a free homogeneous jet of air. The jet is deflected by the sphere, the original angle α changes to the horizontal. The velocity of the jet before deflection V1 = 20 m/s, the cross-sectional area before deflection A1 = 0.25m2. The air density ρ = 1.2 kg/m3.
Viscous forces on the sphere are neglected.

a) Choose a control volume and draw a vector diagram showing the relationship between the force on the jet and the momentum per second entering and leaving the control volume.
b) Calculate the angle α of the jet before deflection.
Calculate c) V2 and d) A2 of the jet after deflection.

Homework Equations


At this point, all of our problems are to be solved using Bernoulli's equation, the Continuity equation and the Momentum equation. (Though I figure that the angle part is just pure trigonometry. :) )

The Attempt at a Solution


For problem b):
My instinct would be to just take the tan-1 of the values opp./adj., as taught by trigonometry. Problem is, I have no idea how to define these values. I did calculate that the force of the flow at the inlet area is 120N assuming that the flow travels horizontally, giving us what could be used as the value for the adjacent side. I'm just not convinced of if this is the correct approach for solving for α, and even if it was, I'm not sure how to proceed with this information.

Any help would be greatly appreciated! Thank you!
Welcome to PF.

For that 120 N force you calculated -- there is a "Δv" involved in that calculation, since you are calculating Δpt. It appears that you have used 20 m/s for Δv. This would be the case if the air jet were brought to a complete stop:
Δv = (20 - 0) m/s ←(Note: NOT TRUE for this problem.)​
However, the jet is not brought to a stop, it is only deflected. So Δv is not the full 20 m/s initial speed of the jet. So, what is Δv in this case, in terms of the angle? Be aware that we are really just interested in one component of Δv (Question: vertical or horizontal?) here.
 
Part (a) calls for you to "choose a control volume and draw a vector diagram showing the relationship between the force on the jet and the momentum per second entering and leaving the control volume." So, let's see it. This diagram was asked for so it can help you solve the problem correctly.

Chet
 
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