Perpendicular Forces Homework: Solving for mg/cos20

AI Thread Summary
The discussion revolves around understanding the forces acting on a wing in a slope scenario, specifically the weight and lift forces. It clarifies that the vertical component of the lift force is calculated using trigonometry, leading to the equation Lift = mg/cos20. Participants highlight the importance of distinguishing between the total lift and its vertical component, which is L cos20. The conversation emphasizes analyzing the vertical forces to ensure equilibrium, where the lift must equal the weight for steady flight. Overall, the key takeaway is the correct application of trigonometric principles to resolve the forces acting on the wing.
ravsterphysics
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The Attempt at a Solution


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I was of the understanding that the slope can be calculated as mgsin20 whereas the force acting straight down through the lift is mgcos20 but the answer is mg divided by cos 20??
 
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Hint: What force components act in the vertical direction? What must they add to?
 
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Doc Al said:
Hint: What force components act in the vertical direction? What must they add to?

in the vertical direction we have weight acting downwards and lift acting upwards? so does it look like this?
2.JPG
 
ravsterphysics said:
in the vertical direction we have weight acting downwards and lift acting upwards?
The weight acts downward. Good! But only a component of the lift force acts vertically. What is that component?
 
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Doc Al said:
The weight acts downward. Good! But only a component of the lift force acts vertically. What is that component?

So only the 'top' part of the weight is what we're after? And the angle is also 20 degrees? So it looks like this?

3.JPG


in which case lift would then be Lift = mg/cos20

I see!

In that case, how does this differ to my notes that say the perpendicular force to the slope would be mgcos20? Is it because we're dealing with a component only?
 
ravsterphysics said:
So only the 'top' part of the weight is what we're after?
Not sure what you mean. There are two forces acting on the wing: Weight, which acts down. And the lift force, which acts at the angle shown.

You need to analyze the vertical components.

ravsterphysics said:
And the angle is also 20 degrees?
The angle that the lift force makes with the vertical is 20 degrees. So what is the vertical component of that force?
 
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Doc Al said:
Not sure what you mean. There are two forces acting on the wing: Weight, which acts down. And the lift force, which acts at the angle shown.

You need to analyze the vertical components.The angle that the lift force makes with the vertical is 20 degrees. So what is the vertical component of that force?

The vertical component is weight (mg) right? So to get lift, we use trig to end up with Lift = mg/cos20? Is that what you mean by vertical component?

4.JPG
 
ravsterphysics said:
The vertical component is weight (mg) right? So to get lift, we use trig to end up with Lift = mg/cos20? Is that what you mean by vertical component?
No. I simply mean: What is the component of the lift force in the vertical direction? You know the angle to the vertical, so how would you find the vertical component? (It will be in terms of L. You'll then use it to solve for L.)
 
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Doc Al said:
No. I simply mean: What is the component of the lift force in the vertical direction? You know the angle to the vertical, so how would you find the vertical component? (It will be in terms of L. You'll then use it to solve for L.)

okay now I'm lost, i thought the mg/cos20 IS the vertical component? if not, can you write it, it'll probably click for me that way.
 
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I hope I'm not adding to your confusion!

ravsterphysics said:
i thought the mg/cos20 IS the vertical component?
Not quite.

ravsterphysics said:
in which case lift would then be Lift = mg/cos20
You had this correct! (Didn't see it earlier.)

But to be clear, here's how to figure out what L is.
(1) vertical component of L = L cos20 (This is what I was trying to get you to say!)
(2) vertical component of weight is just mg (of course, since it's vertical)

ΣFy = 0
L cos20 - mg = 0

Thus:
L cos20 = mg
L = mg/cos20

Does that make sense?
 
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  • #11
ravsterphysics said:
okay now I'm lost, i thought the mg/cos20 IS the vertical component? if not, can you write it, it'll probably click for me that way.
You should start by considering accelerations. You are told the direction of flight is (continuing) horizontal. So in which direction can you be sure there is no acceleration? For that direction, you know that the sum of forces is zero. What is the component of lift in that direction?
 
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