Induced Velocity in Hover, Helicopter Dynamics Lecture 34

Описание к видео Induced Velocity in Hover, Helicopter Dynamics Lecture 34

This video uses momentum theory to derive the expression for the induced velocity at the helicopter rotor disk in hover flight condition. The induced velocity at the rotor disk can be used to estimate power required by the helicopter in hover.
#rotorcraft #helicopter #aerospaceengineering

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