Accession Number : ADA137788

Title :   Calculation of the Aerodynamic Flow Field in the Vicinity of a Sea King Helicopter.

Descriptive Note : Aerodynamics rept.,


Personal Author(s) : Reddy,K R

PDF Url : ADA137788

Report Date : Jun 1983

Pagination or Media Count : 30

Abstract : A mathematical model of the rotor wake in the vicinity of a rotorcraft fuselage is formulated taking into account the mutual interference between the rotor and fuselage. It is assumed that the vortex sheet behind each rotor blade rolls-up into a single, blade tip vortex and that the fuselage can be represented by constant source potential flow panels. The velocity field given by the combined rotor wake and fuselage model is presented for the case of a Sea King helicopter in forward flight. (Author)

Descriptors :   *Wake, *Rotor blades(Rotary wings), Fuselages, Flow separation, Helicopter rotors, Potential flow, Panels, Mathematical prediction, Digital simulation, Interference, Vortices, Flow fields, Mathematical models, Helicopters, Australia

Subject Categories : Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE