Helicopter rotor aeroelastic and aeromechanical stability predictions for four data sets were made using industry and government stability analyses and compared with data at a workshop held at Ames Research Center, August 2-3, 1988. The present report contains the workshop comparisons
In 2006, NASA rotorcraft research was refocused to emphasize high-fidelity first-principles predicti...
Three cases were selected for correlation from an experiment that examined the aeromechanical stabil...
Two cases were selected for correlation from an experiment that examined the aeromechanical stabilit...
Various features of the computer codes used in the helicopter industry and by government agencies fo...
A plan was formed for developing a comprehensive, second-generation system with analytical capabilit...
A number of applications of a rotorcraft aeroelastic analysis are presented to verify that the analy...
Issued as Progress reports [nos. 1-3], and Final report, Project no. E-16-692 (includes subproject E...
Theoretical predictions of aeroelastic stability are compared with experimental, isolated, hingeless...
Theoretical and experimental developments in the aeroelastic and aeromechanical stability of helicop...
The ability of existing data reduction techniques to determine frequency and damping from transient ...
An analytical investigation was conducted to study the influence of various parameters on predicting...
The development and application of comprehensive rotorcraft analysis methods in the field of rotorcr...
A helicopter bearingless main rotor was tested. Areas of investigation included aeroelastic stabilit...
The results of an analytical study aimed at predicting the aeromechanical stability of a helicopter ...
An investigation was conducted in the NASA Langley Transonic Dynamics Tunnel to evaluate an advanced...
In 2006, NASA rotorcraft research was refocused to emphasize high-fidelity first-principles predicti...
Three cases were selected for correlation from an experiment that examined the aeromechanical stabil...
Two cases were selected for correlation from an experiment that examined the aeromechanical stabilit...
Various features of the computer codes used in the helicopter industry and by government agencies fo...
A plan was formed for developing a comprehensive, second-generation system with analytical capabilit...
A number of applications of a rotorcraft aeroelastic analysis are presented to verify that the analy...
Issued as Progress reports [nos. 1-3], and Final report, Project no. E-16-692 (includes subproject E...
Theoretical predictions of aeroelastic stability are compared with experimental, isolated, hingeless...
Theoretical and experimental developments in the aeroelastic and aeromechanical stability of helicop...
The ability of existing data reduction techniques to determine frequency and damping from transient ...
An analytical investigation was conducted to study the influence of various parameters on predicting...
The development and application of comprehensive rotorcraft analysis methods in the field of rotorcr...
A helicopter bearingless main rotor was tested. Areas of investigation included aeroelastic stabilit...
The results of an analytical study aimed at predicting the aeromechanical stability of a helicopter ...
An investigation was conducted in the NASA Langley Transonic Dynamics Tunnel to evaluate an advanced...
In 2006, NASA rotorcraft research was refocused to emphasize high-fidelity first-principles predicti...
Three cases were selected for correlation from an experiment that examined the aeromechanical stabil...
Two cases were selected for correlation from an experiment that examined the aeromechanical stabilit...