NASA NTRS · 19910000214
Calculating Flow Through A Helicopter Rotor
Abstract
New method for calculating flow of air through and around helicopter rotor incorporated into General Rotorcraft Aeromechanical Stability Program (GRASP) (computer program for aeroelastic analysis). Flow about helicopter rotor represented by axisymmetric flow field in cylindrical region with actuator disk as source of flow.
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Kunz, Donald L., Hodges, Dewey H.. 1991-05-01. Calculating Flow Through A Helicopter Rotor. https://ntrs.nasa.gov/citations/19910000214
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