Plane in flight - Dynamics Question

AI Thread Summary
The discussion revolves around calculating the lift and drag forces on a 30,000 kg aircraft climbing at a 15-degree angle with a thrust of 180 kN. Participants express confusion over the use of centripetal acceleration and overall acceleration, clarifying that the given acceleration of 2 m/s² is the total acceleration, not just the increase in speed. The calculations for weight, centripetal force, and lift are debated, with some participants confirming that the approach of separating components is valid. Ultimately, one user confirms their method of calculating lift by subtracting the centripetal force from the resultant force, while still seeking clarity on how to accurately determine drag. The conversation highlights the complexities of applying physics principles to dynamic flight scenarios.
Ryansf98
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Homework Statement


"Figure 5 depicts a 30 000 kg aircraft climbing at an angle θ = 15˚ when the thrust T = 180 kN. The aircraft’s speed is 300 km/hr and its acceleration is 2m/s2. If the radius of curvature of the path is 20 km (i.e., θ is decreasing), compute the lift and drag forces on the aircraft."

a = 2m/s^2
T = 150000N
Theta = 15 degrees
Radius of Curvature (K) = 20000m
v = 300km/hr => v = 83.3 m/s^1

Screenshot (48).png

Homework Equations


W=mg, F=ma, a = v^2/K

The Attempt at a Solution


I was going to treat this similar to an object moving up an inclined plane. Although, I don't know if this would work.

I determined W = mg, W= 294,300N.
I then thought using a = 83.3^2/20000 = 0.35 m/2^1.
Therefore, F = ma, F = 30,000 * 0.35 = 10,500N.

Therefore F + F(f) (i.e. Wsin(Theta)) = Drag.

Upon calculating, I got close to the answer for drag but I believe only by coincidence. As I considered you would have to work out normal and tangential components individually, therefore a= v^2/K would be in the normal direction, not the tangential like I used it for.

I also am unsure on how to calculate Lift if I cannot treat this an incline plane problem.
 
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Ryansf98 said:
I determined W = mg, W= 294,300N.
I then thought using a = 83.3^2/20000 = 0.35 m/2^1.
Therefore, F = ma, F = 30,000 * 0.35 = 10,500N.
I am not sure I understand what you are doing here. Which F is this and in what direction does it point?
 
Ryansf98 said:
F = ma, F = 30,000 * 0.35 = 10,500N.
That 0.35 is using only the centripetal acceleration. You are given an acceleration of 2ms-2,though it is not clear whether that is the overall acceleration or just the increase in speed. Is this F just the net force up the slope?
Ryansf98 said:
F + F(f) (i.e. Wsin(Theta)) = Drag.
I can't make sense of that. Are you saying F(f) stands for W sin(θ)? Doesn't that add to drag? Where is T in that equation?
 
kuruman said:
I am not sure I understand what you are doing here. Which F is this and in what direction does it point?

This is where I was confused, as I was using a incorrectly.

haruspex said:
That 0.35 is using only the centripetal acceleration. You are given an acceleration of 2ms-2,though it is not clear whether that is the overall acceleration or just the increase in speed. Is this F just the net force up the slope?

I tried to use a = v^2/K, but as you both noted I wasn't using it corretly but I don't know how to use it.

So this a would be a(centripetal)? The 2m/s^2 is the overall accleration as far as I'm aware.

[QUOTE="I can't make sense of that. Are you saying F(f) stands for W sin(θ)? Doesn't that add to drag? Where is T in that equation?[/QUOTE]

Yeah that's what I was working there. I was going to determine each component then sum them into a net force at the end.
 
haruspex said:
That 0.35 is using only the centripetal acceleration. You are given an acceleration of 2ms-2,though it is not clear whether that is the overall acceleration or just the increase in speed. Is this F just the net force up the slope?

I can't make sense of that. Are you saying F(f) stands for W sin(θ)? Doesn't that add to drag? Where is T in that equation?

I ended up redoing some of it. I calculated R = 284,272N, then used a(centripetal) = v^2/K, => a = 0.35 m/s^2.

I then used F(centripetal) = ma(centripetal), = 10,408N.

Then I done R - F(centripetal) to calculate lift. I got the answer on the sheet, but is that the correct process?

I also still can't figure out drag.
 
You are given the magnitude of the acceleration vector a = 2 m/s2. You have calculated the centripetal component to be 0.35 m/s2. Can you figure out from these two numbers the acceleration in the direction of motion? Hint: The direction of motion is perpendicular to the centripetal direction.
 
Ryansf98 said:
Then I done R - F(centripetal) to calculate lift. I got the answer on the sheet, but is that the correct process?
Yes. I don't see where you defined R, but it looks like it is W cos(θ). Centripetal is the radial component of the resultant, so =R-lift.
 

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