Discover the Formula for Calculating Static Thrust and RPM Ratio

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    Static Thrust
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Discussion Overview

The discussion focuses on the relationship between thrust and RPM in the context of rotor blades, exploring how to calculate thrust given fixed parameters such as angle of attack and rotor blade area.

Discussion Character

  • Exploratory, Technical explanation, Debate/contested

Main Points Raised

  • One participant seeks a formula to relate thrust to RPM.
  • Another participant asserts that thrust cannot be directly calculated from RPM alone.
  • A different participant asks for a calculation method assuming fixed parameters like angle of attack and rotor blade area.
  • One participant proposes a formula: T=ct half row v square s, though it is unclear how this relates to the previous points.

Areas of Agreement / Disagreement

Participants do not appear to agree on how thrust can be calculated from RPM, with multiple competing views on the relationship and the necessary parameters.

Contextual Notes

The discussion lacks clarity on the definitions of terms used in the proposed formula and the assumptions behind the calculations. There are unresolved aspects regarding the dependencies of thrust on other variables.

rubai
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i want to know the relation between thrust/rpm. what is the formula to calculate it?
 
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You can't directly calculate thrust if all you know is RPMs.
 
If angle of attack and area of rotor blade is fixed how can i calculate it. could you please tell me the calculation of it for fixed parameters.
 
T=ct half row v square s
 

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