Results obtained during the development of a consistent aerodynamic theory for rotors in hovering flight are discussed. Methods of aerodynamic analysis were developed which are adequate for general design purposes until such time as more elaborate solutions become available, in particular solutions which include real fluids effects. Several problems were encountered in the course of this development, and many remain to be solved, however it is felt that a better understanding of the aerodynamic phenomena involved was obtained. Remaining uncertainties are discussed
An experimental research program has been conducted on a series of tilt rotors designed for a range ...
A benchmark test to aid the development of various rotor performance codes was conducted. Simultaneo...
A mathematical model and computer program were implemented to study the main rotor free wake geometr...
Results of computations are presented using vortex sheets to model the wake and test the sensitivity...
Results obtained using a vortex filament model, as opposed to sheets are discussed, against using va...
A number of refinements in the computer code were worked out and tested. Three codes have been writt...
A method was developed which permits the fully coupled calculation of fuselage and rotor airloads fo...
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 unsteady phenomena in the wake of an oscillating wing or rotor blade are examined theoretically ...
The purpose of this research is the development of an unsteady aerodynamic model for rotors such tha...
A triaxial probe and a rotating conventional probe, mounted on a traverse gear operated by two step ...
The experiments with progressing/regressing forced rotor flapping modes have been extended in severa...
Fundamental considerations regarding the theory of modeling of rotary wing airloads, wakes, and aero...
Free wake techniques for performance prediction and optimization of hovering rotor are discussed. Th...
An experimental research program has been conducted on a series of tilt rotors designed for a range ...
A benchmark test to aid the development of various rotor performance codes was conducted. Simultaneo...
A mathematical model and computer program were implemented to study the main rotor free wake geometr...
Results of computations are presented using vortex sheets to model the wake and test the sensitivity...
Results obtained using a vortex filament model, as opposed to sheets are discussed, against using va...
A number of refinements in the computer code were worked out and tested. Three codes have been writt...
A method was developed which permits the fully coupled calculation of fuselage and rotor airloads fo...
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 unsteady phenomena in the wake of an oscillating wing or rotor blade are examined theoretically ...
The purpose of this research is the development of an unsteady aerodynamic model for rotors such tha...
A triaxial probe and a rotating conventional probe, mounted on a traverse gear operated by two step ...
The experiments with progressing/regressing forced rotor flapping modes have been extended in severa...
Fundamental considerations regarding the theory of modeling of rotary wing airloads, wakes, and aero...
Free wake techniques for performance prediction and optimization of hovering rotor are discussed. Th...
An experimental research program has been conducted on a series of tilt rotors designed for a range ...
A benchmark test to aid the development of various rotor performance codes was conducted. Simultaneo...
A mathematical model and computer program were implemented to study the main rotor free wake geometr...