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Derivation of the Aerodynamic Forces for the Mesicopter Simulation Gary Fay February 14, 2001 This document describes the derivation of the aerodynamic forces used in the equations of motion for stability and control ana
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Document Date: 2001-02-21 15:44:07
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File Size: 93,46 KB
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closed form solution /
energy /
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UT UP /
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Utah /
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Technology
Simulation /
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Fluid mechanics
Helicopter
Blade element theory
Drag
Turbine
Helicopter rotor
Wind turbine aerodynamics
Aerospace engineering
Aerodynamics
Fluid dynamics