Add to ORKGResults of computations are presented using vortex sheets to model the wake and test the sensitivity of the solutions to various assumptions used in the development of the models. The complete codings are included
The aim of this effort was to develop a comprehensive performance optimization capability for tiltro...
A user's manual is presented for a computer program in which a vortex-lattice lifting-surface method...
A benchmark test to aid the development of various rotor performance codes was conducted. Simultaneo...
Results obtained using a vortex filament model, as opposed to sheets are discussed, against using va...
Results obtained during the development of a consistent aerodynamic theory for rotors in hovering fl...
A method was developed which permits the fully coupled calculation of fuselage and rotor airloads fo...
Rotor wake geometries are predicted by a process similar to the startup of a rotor in a free stream....
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.Ti...
A number of refinements in the computer code were worked out and tested. Three codes have been writt...
A mathematical model and computer program was implemented to study the main rotor free wake geometry...
A triaxial probe and a rotating conventional probe, mounted on a traverse gear operated by two step ...
An experimental investigation was conducted in the Langley 14- by 22-Foot Subsonic Tunnel to quantif...
The development of an advanced computational analysis of unsteady aerodynamic loads on isolated heli...
The roll-up of a vortex sheet is analyzed by two approaches. The first is based on exact compressibl...
Free wake techniques for performance prediction and optimization of hovering rotor are discussed. Th...
The aim of this effort was to develop a comprehensive performance optimization capability for tiltro...
A user's manual is presented for a computer program in which a vortex-lattice lifting-surface method...
A benchmark test to aid the development of various rotor performance codes was conducted. Simultaneo...
Results obtained using a vortex filament model, as opposed to sheets are discussed, against using va...
Results obtained during the development of a consistent aerodynamic theory for rotors in hovering fl...
A method was developed which permits the fully coupled calculation of fuselage and rotor airloads fo...
Rotor wake geometries are predicted by a process similar to the startup of a rotor in a free stream....
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.Ti...
A number of refinements in the computer code were worked out and tested. Three codes have been writt...
A mathematical model and computer program was implemented to study the main rotor free wake geometry...
A triaxial probe and a rotating conventional probe, mounted on a traverse gear operated by two step ...
An experimental investigation was conducted in the Langley 14- by 22-Foot Subsonic Tunnel to quantif...
The development of an advanced computational analysis of unsteady aerodynamic loads on isolated heli...
The roll-up of a vortex sheet is analyzed by two approaches. The first is based on exact compressibl...
Free wake techniques for performance prediction and optimization of hovering rotor are discussed. Th...
The aim of this effort was to develop a comprehensive performance optimization capability for tiltro...
A user's manual is presented for a computer program in which a vortex-lattice lifting-surface method...
A benchmark test to aid the development of various rotor performance codes was conducted. Simultaneo...