The development and application of comprehensive rotorcraft analysis methods in the field of rotorcraft technology are described. These large scale analyses and the resulting computer programs are intended to treat the complex aeromechanical phenomena that describe the behavior of rotorcraft. They may be used to predict rotor aerodynamics, acoustic, performance, stability and control, handling qualities, loads and vibrations, structures, dynamics, and aeroelastic stability characteristics for a variety of applications including research, preliminary and detail design, and evaluation and treatment of field problems. The principal comprehensive methods developed or under development in recent years and generally available to the rotorcraft co...
A NASA Langley-sponsored rotorcraft structural dynamics program, known as Design Analysis Methods fo...
Helicopter rotor aeroelastic and aeromechanical stability predictions for four data sets were made u...
The NASA Langley Research Center in 1984 initiated a rotorcraft structural dynamics program, designa...
AbstractThe history, status and lessons of a comprehensive analysis for rotorcraft are reviewed. The...
The history, status, and lessons of a comprehensive analysis for rotorcraft are reviewed. The develo...
An assessment of the status of helicopter theory and analysis is presented. The technology level emb...
Results from the comprehensive analysis CAMRAD II are presented, illustrating recent developments in...
Results from the comprehensive analysis CAMRAD II are presented, illustrating recent developments in...
The unique demands of rotorcraft aeromechanics analysis have led to the development of software tool...
Various features of the computer codes used in the helicopter industry and by government agencies fo...
The use of a computer program for a comprehensive analytical model of rotorcraft aerodynamics and dy...
A number of applications of a rotorcraft aeroelastic analysis are presented to verify that the analy...
Rapid advances in the technology of electronic digital computers and the need for an integrated synt...
A plan was formed for developing a comprehensive, second-generation system with analytical capabilit...
Over fifty years of contributions by NASA and the Army through rotor systems flight research were ex...
A NASA Langley-sponsored rotorcraft structural dynamics program, known as Design Analysis Methods fo...
Helicopter rotor aeroelastic and aeromechanical stability predictions for four data sets were made u...
The NASA Langley Research Center in 1984 initiated a rotorcraft structural dynamics program, designa...
AbstractThe history, status and lessons of a comprehensive analysis for rotorcraft are reviewed. The...
The history, status, and lessons of a comprehensive analysis for rotorcraft are reviewed. The develo...
An assessment of the status of helicopter theory and analysis is presented. The technology level emb...
Results from the comprehensive analysis CAMRAD II are presented, illustrating recent developments in...
Results from the comprehensive analysis CAMRAD II are presented, illustrating recent developments in...
The unique demands of rotorcraft aeromechanics analysis have led to the development of software tool...
Various features of the computer codes used in the helicopter industry and by government agencies fo...
The use of a computer program for a comprehensive analytical model of rotorcraft aerodynamics and dy...
A number of applications of a rotorcraft aeroelastic analysis are presented to verify that the analy...
Rapid advances in the technology of electronic digital computers and the need for an integrated synt...
A plan was formed for developing a comprehensive, second-generation system with analytical capabilit...
Over fifty years of contributions by NASA and the Army through rotor systems flight research were ex...
A NASA Langley-sponsored rotorcraft structural dynamics program, known as Design Analysis Methods fo...
Helicopter rotor aeroelastic and aeromechanical stability predictions for four data sets were made u...
The NASA Langley Research Center in 1984 initiated a rotorcraft structural dynamics program, designa...