Question: Helicopter over a scale

  • Context: High School 
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    Helicopter Scale
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Discussion Overview

The discussion revolves around the scenario of a helicopter taking off from a scale, specifically focusing on the force registered by the scale at the moment the helicopter leaves it. Participants explore the dynamics of lift, weight, and the timing of forces involved in the takeoff process.

Discussion Character

  • Debate/contested
  • Technical explanation
  • Mathematical reasoning

Main Points Raised

  • One participant asserts that the scale must register at least 6868 N when the helicopter leaves the scale, based on the requirement for the helicopter to produce lift greater than its weight.
  • Another participant requests clarification on the reasoning behind the initial claim, indicating a desire to understand the thought process without influencing the discussion.
  • A different viewpoint suggests that the scale's reading depends on the vertical force applied to the helicopter just before takeoff and the time it takes for that force to affect the scale.
  • One participant emphasizes the need to consider secondary effects, such as the mass of the air and the rotor's acceleration, which may influence the scale's reading at the moment of takeoff.

Areas of Agreement / Disagreement

Participants do not appear to reach a consensus, as multiple competing views on the scale's reading at takeoff are presented, and the discussion remains unresolved.

Contextual Notes

The discussion highlights the complexity of the scenario, including the timing of forces and the influence of air dynamics, which may not be fully accounted for in the initial reasoning.

HawkHunt
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Hey all,

This is clearly a very simple question but for some reason my roommate and I just can't agree on this.

The scenario is as follows: There is a helicopter sitting on a scale. The helicopter weighs 700kg and thus has 700*g = 6867 N of force acting on it by gravity. In order to fly the helicopter must overcome its own weight and so it must produce >6867N of lift.

The question is, how much does the scale register on the millisecond the helicopter leaves the scale. My reasoning is that the scale must register 6868N atleast.

Please enlighten me.
 
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It would help if you told us why you think that. I have a theory that might not be correct, but I'd like to hear your thoughts first, so as to not poison the water.
 
Assuming the scale is fully supporting the downstream or air, it would depend on the vertical force applied to the helicopter during the period leading up to T+0.001 seconds and the time it takes for that force to be transferred through the air.

If the rotor generated 0 lift at T=-0.0001 and 2G's starting at T=0, then the scale would likely register 0 at T=0.001 - because no downdraft would have been generated in time to reach the scale that soon.
 
HawkHunt said:
The question is, how much does the scale register on the millisecond the helicopter leaves the scale. My reasoning is that the scale must register 6868N atleast.
F=ma. :smile:

(with what vertical acceleration does the helo leave the pad?)
 
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berkeman said:
F=ma. :smile:

(with what vertical acceleration does the helo leave the pad?)
@HawkHunt did not pose this question in the classical way - that is, as a steady state problem. So secondary effects (like the mass of the air and how quickly the rotor has spun up) need to be considered as well.
 

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