Decoding Helicopter Movement: The Equation Behind Vertical Flight

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Discussion Overview

The discussion revolves around the fundamental equations governing the vertical movement of a helicopter, specifically focusing on the relationship between rotor dynamics and lift generation. Participants explore the mechanics of helicopter flight in one dimension, emphasizing the role of angular acceleration and mass in achieving vertical lift.

Discussion Character

  • Exploratory, Technical explanation, Conceptual clarification

Main Points Raised

  • One participant inquires about the major equation that determines if a disc with specific radius and angular acceleration can lift a given mass vertically.
  • Another participant suggests that a helicopter rotor blade functions similarly to a wing, indicating that the speed of the blade is influenced by its radius and RPM, which in turn affects lift calculation.
  • A request for the specific equation related to lift is made by a participant seeking further clarification.
  • A link to an external resource on lift equations is provided by another participant, possibly as a reference for the requested information.

Areas of Agreement / Disagreement

Participants do not reach a consensus on the specific equation needed for the discussion, and multiple viewpoints regarding the mechanics of helicopter lift are presented without resolution.

Contextual Notes

There are limitations in the discussion regarding the assumptions made about the relationship between rotor dynamics and lift, as well as the dependence on definitions of terms like "angular acceleration" and "mass." The mathematical steps required to derive the lift equation remain unresolved.

Moses
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Well, I know this Q might look cheesy or silly...but:
What is the major equation which decides if X disc with Y raduis with Z angular acceleration will carry M mass and "fly" with it...I am just concern about vertical movements...not the horizantal...Basically its about a hgelicopter moving in one dimension "up"

Cheerz
 
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I'm not sure about your wording there, but a helicopter rotor blade is just a wing. The speed of the blade at any point depends on its radius and rpm, then with that, you can calculate the lift.
 
Can you give me the equation of the left please?

Thx for help.
 

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