Add to ORKGA mathematical model and computer program was implemented to study the main rotor free wake geometry effects on helicopter rotor blade air loads and response in steady maneuvers. Volume 1 (NASA CR-2110) contains the theoretical formulation and analysis of results. Volume 2 contains the computer program listing
Computer program listings are presented for two separate programs: the wake geometry 1 blade loads a...
Results obtained during the development of a consistent aerodynamic theory for rotors in hovering fl...
This User's Manual was prepared to provide the engineer with the information required to run the cou...
A mathematical model and computer program were implemented to study the main rotor free wake geometr...
Rotor wake geometries are predicted by a process similar to the startup of a rotor in a free stream....
A method was developed which permits the fully coupled calculation of fuselage and rotor airloads fo...
Isometric and projection view plots, inflow ratio nomographs, undistorted axial displacement nomogra...
Results obtained using a vortex filament model, as opposed to sheets are discussed, against using va...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.Ti...
Results of computations are presented using vortex sheets to model the wake and test the sensitivity...
The use of a computer program for a comprehensive analytical model of rotorcraft aerodynamics and dy...
Computer program for calculating effects of swash-plate stiffness on helicopter rotor system dynamic...
The development of an advanced computational analysis of unsteady aerodynamic loads on isolated heli...
The Rotor-Fuselage Analysis is a method of calculating the aerodynamic reaction between a helicopter...
An efficient state-of-the-art method was developed to determine the unteady vibratory airloads produ...
Computer program listings are presented for two separate programs: the wake geometry 1 blade loads a...
Results obtained during the development of a consistent aerodynamic theory for rotors in hovering fl...
This User's Manual was prepared to provide the engineer with the information required to run the cou...
A mathematical model and computer program were implemented to study the main rotor free wake geometr...
Rotor wake geometries are predicted by a process similar to the startup of a rotor in a free stream....
A method was developed which permits the fully coupled calculation of fuselage and rotor airloads fo...
Isometric and projection view plots, inflow ratio nomographs, undistorted axial displacement nomogra...
Results obtained using a vortex filament model, as opposed to sheets are discussed, against using va...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.Ti...
Results of computations are presented using vortex sheets to model the wake and test the sensitivity...
The use of a computer program for a comprehensive analytical model of rotorcraft aerodynamics and dy...
Computer program for calculating effects of swash-plate stiffness on helicopter rotor system dynamic...
The development of an advanced computational analysis of unsteady aerodynamic loads on isolated heli...
The Rotor-Fuselage Analysis is a method of calculating the aerodynamic reaction between a helicopter...
An efficient state-of-the-art method was developed to determine the unteady vibratory airloads produ...
Computer program listings are presented for two separate programs: the wake geometry 1 blade loads a...
Results obtained during the development of a consistent aerodynamic theory for rotors in hovering fl...
This User's Manual was prepared to provide the engineer with the information required to run the cou...