Add to ORKGA lifting surface theory has been developed for a helicopter rotor in forward flight for incompressible flow. The method utilized the concept of the linearized acceleration potential and make use of the vortex lattice procedures. Results in terms of lift coefficient slope for several forward flight conditions are given
Isometric and projection view plots, inflow ratio nomographs, undistorted axial displacement nomogra...
In this study, the helicopter blade in forward-flight condition was investigated. The blade element ...
The wake information from a helicopter forward flight code is coupled with two transonic potential r...
A lifting surface theory was developed for a helicopter rotor in forward flight for compressible and...
This thesis is concerned with the development of a theory for determining the aerodynamic forces for...
A theoretical analysis indicates that, for rotors, ground effect decreases rapidly with increases in...
Theor,.t;eally d_rir_d,wpr_,_,_'i(ms fl_r the flapping, the thrust, the torque, a,d tt, _ yrqfi...
Theoretical derived expressions for the flapping, the thrust, the torque, and the profile drag-lift ...
Since the author has always been interested in Aeronautical Engineering, and in particular, rotary-w...
The purpose of this research is the development of an unsteady aerodynamic model for rotors such tha...
AbstractThe approach of inner/outer fields is applied in order to calculate the aerodynamic loads at...
The development of an advanced computational analysis of unsteady aerodynamic loads on isolated heli...
a summary is given of the principal results on air forces for a wing undergoing unsteady motion in a...
An overset grid thin-layer Navier-Stokes code has been extended to include dynamic motion of helicop...
Vita.The application of numerical lifting surface theory to the calculation of rotor hover performan...
Isometric and projection view plots, inflow ratio nomographs, undistorted axial displacement nomogra...
In this study, the helicopter blade in forward-flight condition was investigated. The blade element ...
The wake information from a helicopter forward flight code is coupled with two transonic potential r...
A lifting surface theory was developed for a helicopter rotor in forward flight for compressible and...
This thesis is concerned with the development of a theory for determining the aerodynamic forces for...
A theoretical analysis indicates that, for rotors, ground effect decreases rapidly with increases in...
Theor,.t;eally d_rir_d,wpr_,_,_'i(ms fl_r the flapping, the thrust, the torque, a,d tt, _ yrqfi...
Theoretical derived expressions for the flapping, the thrust, the torque, and the profile drag-lift ...
Since the author has always been interested in Aeronautical Engineering, and in particular, rotary-w...
The purpose of this research is the development of an unsteady aerodynamic model for rotors such tha...
AbstractThe approach of inner/outer fields is applied in order to calculate the aerodynamic loads at...
The development of an advanced computational analysis of unsteady aerodynamic loads on isolated heli...
a summary is given of the principal results on air forces for a wing undergoing unsteady motion in a...
An overset grid thin-layer Navier-Stokes code has been extended to include dynamic motion of helicop...
Vita.The application of numerical lifting surface theory to the calculation of rotor hover performan...
Isometric and projection view plots, inflow ratio nomographs, undistorted axial displacement nomogra...
In this study, the helicopter blade in forward-flight condition was investigated. The blade element ...
The wake information from a helicopter forward flight code is coupled with two transonic potential r...