Title: Rotorcraft Wake Analysis for the Prediction of Induced Velocities
Abstract: Abstract : A rotorcraft wake analysis for computing flow velocities induced by the rotors and wing of a helicopter is described, and predicted induced velocities are compared with experimental data from many sources. Combined in a single computerized analysis are the capabilities for calculating three components of time-averaged and instantaneous induced velocities on or off the rotor(s) of single-rotor, dual-rotor, and winged helicopter configurations in hovering and forward flight.
Publication Year: 1976
Publication Date: 1976-01-01
Language: en
Type: report
Indexed In: ['crossref']
Access and Citation
Cited By Count: 20
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