The problems that were encountered in the dynamics of advanced rotor systems are described. The methods for analyzing these problems are discussed, as are past solutions of the problems. To begin, the basic dynamic problems of rotors are discussed: aeroelastic stability, rotor and airframe loads, and aircraft vibration. Next, advanced topics that are the subject of current research are described: vibration control, dynamic upflow, finite element analyses, and composite materials. Finally, the dynamics of various rotorcraft configurations are considered: hingeless rotors, bearingless rotors, rotors with circulation control, coupled rotor/engine dynamics, articulated rotors, and tilting proprotor aircraft
The paper will review the development and application of the mathematical modelling of the advanced ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76177/1/AIAA-9022-592.pd
The results of an analytical study aimed at predicting the aeromechanical stability of a helicopter ...
The dynamic structural analysis of rotary winged aircraft is reported, considering helicopter vibrat...
Theoretical and experimental developments in the aeroelastic and aeromechanical stability of helicop...
A number of applications of a rotorcraft aeroelastic analysis are presented to verify that the analy...
The requirement for low vibrations has achieved the status of a critical design consideration in mod...
An an overview and discussion of those aspects of airframe structural dynamics that have a strong in...
The rotor dynamic design considerations are essentially limitations on the vibratory response of the...
An analytical investigation was conducted to study the influence of various parameters on predicting...
This book is the result of almost 30 years of work in the field of rotordynamics, which includes res...
A linearized model of rotorcraft dynamics has been developed through the use of symbolic automatic e...
An overview of the methods and concepts developed to enhance and predict structural dynamic characte...
The effects of three gyroless rotor feedback systems: (1) coning feedback, (2) proportional tilting ...
The paper will review the development and application of the mathematical modelling of the advanced ...
The paper will review the development and application of the mathematical modelling of the advanced ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76177/1/AIAA-9022-592.pd
The results of an analytical study aimed at predicting the aeromechanical stability of a helicopter ...
The dynamic structural analysis of rotary winged aircraft is reported, considering helicopter vibrat...
Theoretical and experimental developments in the aeroelastic and aeromechanical stability of helicop...
A number of applications of a rotorcraft aeroelastic analysis are presented to verify that the analy...
The requirement for low vibrations has achieved the status of a critical design consideration in mod...
An an overview and discussion of those aspects of airframe structural dynamics that have a strong in...
The rotor dynamic design considerations are essentially limitations on the vibratory response of the...
An analytical investigation was conducted to study the influence of various parameters on predicting...
This book is the result of almost 30 years of work in the field of rotordynamics, which includes res...
A linearized model of rotorcraft dynamics has been developed through the use of symbolic automatic e...
An overview of the methods and concepts developed to enhance and predict structural dynamic characte...
The effects of three gyroless rotor feedback systems: (1) coning feedback, (2) proportional tilting ...
The paper will review the development and application of the mathematical modelling of the advanced ...
The paper will review the development and application of the mathematical modelling of the advanced ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76177/1/AIAA-9022-592.pd
The results of an analytical study aimed at predicting the aeromechanical stability of a helicopter ...