Calculate Thrust Force of Aero Modeling

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    Calculation Thrust
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SUMMARY

The discussion centers on calculating the thrust force of an aero modeling project, specifically using propeller diameter and RPM to derive air velocity. A user seeks assistance in determining the air velocity necessary for thrust calculations. The recommended approach involves applying Bernoulli's principle for an idealized rotor disc to facilitate these calculations. For further guidance, the user is directed to a NASA resource on propeller thrust.

PREREQUISITES
  • Understanding of Bernoulli's principle in fluid dynamics
  • Familiarity with propeller mechanics and aerodynamics
  • Basic knowledge of thrust force calculations
  • Ability to interpret RPM and its impact on thrust
NEXT STEPS
  • Research Bernoulli's equation and its application to rotor dynamics
  • Learn how to calculate thrust using propeller diameter and RPM
  • Explore computational fluid dynamics (CFD) tools for thrust analysis
  • Investigate the NASA resource on propeller thrust for practical examples
USEFUL FOR

Aerospace engineers, aerodynamics researchers, and hobbyists involved in aero modeling projects will benefit from this discussion.

vijayvelprakash
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thrust calculation...

am doing an analysis with the aero modelling as part of my project...
i need to calculate the thrust force of the aero...i have the propeller diameter and rpm...i need the air velocity that comes out from the propeller to calculate the thrust... but i don't know how to claculate the air velocity... anyone who has a solution please post ur solution quickly as it is really urgent!
 
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