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Revolutionary
Tapered Scimitar
Rotor Design

 
 
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Technical Merit

 
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Computational Fluid Dynamics (CFD)

We have preliminarily verified aerodynamic and acoustic performance utilizing the Computational Fluid Dynamic (CFD) Program ANSYS

 
 
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CFD Thrust Chart

CFD shows us thrust and torque generation in Newtons. We can then evaluate the power required.

Thrust 2000 N

Torque 525 N = 44 KWH @ 800 RPMS

= 22 KWH for 30 Min Flight

This evolution in rotor design was years in the making.

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The Inefficiency of the Modern Rotor

Speed vs. Thrust

This graph shows actual lift/thrust versus calculated maximum lift/thrust that a ideal rotor system should have with 100% efficiency. What is shown are the approximations, the source show's a more accurate depiction . Source: https://collections.lib.utah.edu/dl_files/5d/e4/5de41dbc5c175875bdf296d0600a3ffff3d4d522.pdf (pg. 51)