Fundamental considerations regarding the theory of modeling of rotary wing airloads, wakes, and aeroelasticity are presented. The topics covered are: airloads and wakes, including lifting-line theory, wake models and nonuniform inflow, free wake geometry, and blade-vortex interaction; aerodynamic and wake models for aeroelasticity, including two-dimensional unsteady aerodynamics and dynamic inflow; and airloads and structural dynamics, including comprehensive airload prediction programs. Results of calculations and correlations are presented
AbstractTwo methods for calculating the wake geometry and blade loads for a hovering helicopter roto...
A Computational Fluid Dynamics (CFD) analysis is developed for 3-D rotor unsteady aerodynamic load p...
Rotor wake geometries are predicted by a process similar to the startup of a rotor in a free stream....
Thesis. 1975. Ph.D.--Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.Vi...
An analytic investigation to generalize wake geometry of a helicopter rotor in steady level forward ...
A mathematical model and computer program were implemented to study the main rotor free wake geometr...
The unsteady loads experienced by a helicopter are known to be strongly influenced by aerodynamic in...
The unsteady loads experienced by a helicopter are known to be strongly influenced by aerodynamic in...
The unsteady loads experienced by a helicopter are known to be strongly influenced by aerodynamic in...
The unsteady loads experienced by a helicopter are known to be strongly influenced by aerodynamic in...
The dynamic structural analysis of rotary winged aircraft is reported, considering helicopter vibrat...
The development of an advanced computational analysis of unsteady aerodynamic loads on isolated heli...
Rotor wake geometries are predicted by a process similar to the startup of a rotor in a free stream....
The purpose of this research is the development of an unsteady aerodynamic model for rotors such tha...
Comparisons of measured and calculated aerodynamic behavior of a tiltrotor model are presented. The ...
AbstractTwo methods for calculating the wake geometry and blade loads for a hovering helicopter roto...
A Computational Fluid Dynamics (CFD) analysis is developed for 3-D rotor unsteady aerodynamic load p...
Rotor wake geometries are predicted by a process similar to the startup of a rotor in a free stream....
Thesis. 1975. Ph.D.--Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.Vi...
An analytic investigation to generalize wake geometry of a helicopter rotor in steady level forward ...
A mathematical model and computer program were implemented to study the main rotor free wake geometr...
The unsteady loads experienced by a helicopter are known to be strongly influenced by aerodynamic in...
The unsteady loads experienced by a helicopter are known to be strongly influenced by aerodynamic in...
The unsteady loads experienced by a helicopter are known to be strongly influenced by aerodynamic in...
The unsteady loads experienced by a helicopter are known to be strongly influenced by aerodynamic in...
The dynamic structural analysis of rotary winged aircraft is reported, considering helicopter vibrat...
The development of an advanced computational analysis of unsteady aerodynamic loads on isolated heli...
Rotor wake geometries are predicted by a process similar to the startup of a rotor in a free stream....
The purpose of this research is the development of an unsteady aerodynamic model for rotors such tha...
Comparisons of measured and calculated aerodynamic behavior of a tiltrotor model are presented. The ...
AbstractTwo methods for calculating the wake geometry and blade loads for a hovering helicopter roto...
A Computational Fluid Dynamics (CFD) analysis is developed for 3-D rotor unsteady aerodynamic load p...
Rotor wake geometries are predicted by a process similar to the startup of a rotor in a free stream....