How to calculate tension in a cable

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    Cable Tension
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Discussion Overview

The discussion revolves around calculating the tension in a cable when an aircraft drops a load that remains attached by the cable. Participants explore various scenarios involving the angle of the cable, the effects of drag, and the dynamics of the load as it is released. The conversation includes theoretical considerations and practical implications related to the forces acting on the system.

Discussion Character

  • Exploratory
  • Technical explanation
  • Debate/contested
  • Mathematical reasoning

Main Points Raised

  • One participant asks how to calculate the tension given the aircraft speed, load weight, and cable length, without knowing the angle of the cable.
  • Another participant suggests that knowing the angle of the cable with respect to the vertical would simplify the calculation.
  • A participant proposes calculating tension at specific angles, such as 90 degrees to the vertical and 30 degrees below the horizontal.
  • Concerns are raised about the impossibility of the cable reaching a horizontal position without resulting in infinite tension.
  • Some participants discuss the effects of drag on the load and cable, noting that the string may not be vertical due to the load retaining its horizontal velocity component.
  • It is mentioned that the drag on the cable could lead to a curve, and while the tension is constant, the shape of the cable may not be a perfect catenary.
  • Participants highlight the importance of knowing the size and shape of the load to estimate drag accurately, as well as the altitude of the aircraft.
  • One participant speculates about the possibility of the load generating lift or buoyancy, which could affect the tension calculation.
  • There is a discussion about the relationship between air resistance and the angle of the cable, with suggestions that it could be modeled as either a catenary or a parabola depending on the conditions.
  • A participant warns that at high speeds, the dynamics of the load dropping could lead to unexpected outcomes, emphasizing the role of drag coefficient.

Areas of Agreement / Disagreement

Participants express multiple competing views regarding the effects of drag, the behavior of the cable, and the conditions under which tension can be calculated. The discussion remains unresolved, with no consensus on the best approach to the problem.

Contextual Notes

Limitations include the lack of specific information about the drag coefficient of the load, the angle of the cable, and the assumptions made about air resistance. The discussion also highlights the complexity of modeling the cable's behavior under varying conditions.

twinplums
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If an aircraft is flying straight and level and drops a load but it remains attatched to the aircraft by a cable (hung load), how do I calculate the tension in the cable. I know the aircraft speed, the weight og the load and the length of the cable.

Thanks
 
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twinplums said:
If an aircraft is flying straight and level and drops a load but it remains attatched to the aircraft by a cable (hung load), how do I calculate the tension in the cable. I know the aircraft speed, the weight og the load and the length of the cable.

Thanks

Welcome to the PF.

Do you also have the angle that the cable makes with the vertical? That would help a lot in simplifying the calculation.
 
Thanks,

I do not know an angle as it is only theoretical,

but I would like to know how to calculate 90deg to the vertical i.e. directly behind the aircraft and

a 30deg below the horizontal
 
It can never get to horizontal. The tension would be unlimited.
At θ to the vertical, we have
Vertical load = L
Horizontal load (drag) = H
Tension = T = sqrt(H^2+L^2)
tan(θ) = H/L
cos(θ) = L/T
So T = L.sec(θ).
At 30 degrees, T = 2L/√3
 
Won't the string be vertical? The load on board the plane has the same horizontal velocity component as the plane, and will retain this velocity component as it is lowered. [I'm appealing to Newton's first law (the law of inertia).]

Edit: I was being silly. Air resistance will, of course, be significant.
 
Last edited:
Philip Wood said:
Won't the string be vertical? The load on board the plane has the same horizontal velocity component as the plane, and will retain this velocity component as it is lowered. [I'm appealing to Newton's first law (the law of inertia).]

I would expect drag to be significant, so the string will trail.
In fact, drag on the string may be important, so it won't even be straight. But if you only care about the max tension, the angle at the top of the string should give the right answer.
 
Yes, typically, you get a curve, because the drag on the cable adds up, but the tension is constant throughout. Won't be quite catenary, but should be close. If weight is heavy and provides significant drag, however, straight line will give reasonable approximation.
 
Thank you for your replies,

The aircraft speed is 390 km per h, the load is 90Kg and the cable is 1.5 meters.
 
In the unlikely event that air resistance is much smaller than the weight of the load (883 N), then the cable will hang almost vertically, and the tension in it will be approximately 883 N.

If air resistance isn't negligible (compared with 883 N), we need to know how large it is. It can't be estimated knowing the speed of the plane, unless we know the size and shape of the load. Even then, it would be no easy matter.
 
  • #10
Yes, shape and size of the load can be used to estimate drag. Altitude will also matter. Cable is short enough for the curving to be insignificant, so it can be estimated as a straight line.
 
  • #11
haruspex said:
It can never get to horizontal. The tension would be unlimited.

Not necessarily. The object beinig towed might be generating a lift or buoyancy force, so its weight is zero or even negative. This applies to an aircraft towing a sailplane (glider) for example.
 
  • #12
K^2 said:
Yes, typically, you get a curve, because the drag on the cable adds up, but the tension is constant throughout. Won't be quite catenary, but should be close. If weight is heavy and provides significant drag, however, straight line will give reasonable approximation.
Depends how the air resistance depends on the angle of the section of cable.
If the air resistance is constant per unit length of cable (i.e. not affected by the angle) then it would be a catenary. If, at the opposite extreme, it only depends on the vertical length of each section of cable then it would be a parabola. So I'd guess something between the two.
 
  • #13
twinplums said:
Thank you for your replies,

The aircraft speed is 390 km per h, the load is 90Kg and the cable is 1.5 meters.

Hmm.. at that speed and short cable length you could get a nasty surprise.
As it drops, it will take a short time for the air resistance to retard it relative to the plane. If the cable becomes taut before that process completes it will then swing upwards and may strike the underbelly. It's all going to depend on the drag coefficient of the object. How dense is it?
 
  • #14
haruspex said:
Depends how the air resistance depends on the angle of the section of cable.
If the air resistance is constant per unit length of cable (i.e. not affected by the angle) then it would be a catenary. If, at the opposite extreme, it only depends on the vertical length of each section of cable then it would be a parabola. So I'd guess something between the two.
That's basically what I was thinking. Though, I didn't think to establish the second limiting case. Good call on the parabola. Yes, it'd be somewhere in between these two. It's probably worth pointing out that a short segment of a catenary is well-approximated by a parabolic segment.
 

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