Two Ducted Fans For More Thrust

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SUMMARY

The discussion centers on the effectiveness of using two ducted fans, each powered by its own motor, to enhance thrust in a cylindrical design. The primary focus is on the configuration where one fan is located at the intake and the other at the exhaust, potentially leading to increased thrust through super-acceleration of air. Key considerations include the diameter of the fans, which should be at least 12 inches, and the importance of the pressure ratio between the two fans. Preliminary actuator disk theory analysis is recommended for evaluating performance outcomes.

PREREQUISITES
  • Understanding of ducted fan mechanics
  • Familiarity with actuator disk theory
  • Knowledge of pressure ratios in fluid dynamics
  • Experience with motor control for fan RPM management
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  • Research actuator disk theory analysis techniques
  • Explore the impact of pressure ratios on ducted fan performance
  • Investigate fixed-speed axial fan characteristics
  • Learn about optimizing thrust in ducted fan systems
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Aerospace engineers, hobbyists designing UAVs, and anyone interested in optimizing thrust using ducted fan configurations.

rembrandtgos
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If you have a cylinder with a slightly larger diameter at one end (the intake end) Would having one ducted fan powered by it's own motor at intake end and a second ducted fan powered by it's own motor at the exhaust end produce more thrust? It seems like the already accelerated air coming from the intake fan would be "super accelerated" by the exhaust ducted fan? I purposely stated using two fans for reasons of experimenting/controlling fan RPMs separately and also my final design may not be a straight cylinder. The diameter of fans would probably need to be at least 12 inches for the power I'd need. Any suggestions by folks with real experience with larger ducted fans would greatly be appreciated.
 
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It depends on the the fans and duct. If the fans are fixed-speed axial and the pressure drop is low, there won't be much of an impact.
 
One thing you need to know, as was stated earlier, is the pressure ratio of the two fans. You can perform a preliminary actuator disk theory analysis
 

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