Search
Now showing items 1-1 of 1
A discrete vortex model for the calculation of aerodynamic loads on a blade of a N-bladed helicopter rotor in rectilinear flight
(Stellenbosch : Stellenbosch University, 1992)
ENGLISH ABSTRACT: A model for the calculation of aerodynamic loads on a blade of a n-bladed helicopter rotor
in rectilinear flight was developed and computerized. The model is based on a lifting line
blade representation ...