Mutual interference between rotors, wing, and tail of helicopter has large effect upon overall performance and stability of aircraft; equations are developed for all three induced velocity components at arbitrary point and for arbitrary harmonic of vorticity distribution.
Equations for induced velocities near lifting rotor with nonuniform azimuthwise vorticity distribution
NASA -- Tech Note
1960
25 pages
Report
English
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Charts of induced velocities near lifting rotor
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