Add to ORKGRotor-hub bending moment measurements on hingeless rotor helicopter during abrupt maneuvers near groun
A full-scale BO-105 hingeless rotor system was tested in the NASA Ames 40- by 80-Foot Wind Tunnel on...
The present report is a study of the dynamic stability of a helicopter with hinged rotor blades unde...
Data from 23 flight conditions, including level flights ranging from advance ratio mu = 0.14 to 0.37...
Flight tests on hingeless rotor compound helicopter to determine level flight and maneuvering charac...
Flight test and analysis of structural loads in helicopter hingeless rotor syste
Flight investigation of control qualities of rudimentary hingeless rotor helicopte
Flight tests have been conducted with a single-rotor helicopter, one blade of which was equipped at ...
A two-blade rotor having a diameter of 4 feet and a solidity of 0.037 was tested in the Langley 300-...
The source of an appreciable pitching-moment difference between left and right hovering turns for a ...
Flight investigations of wing-rotor lift-sharing characteristics of XH-51 helicopte
A study was conducted in which available airload and blade response data for the NH-3A and CH-53A ro...
Wind tunnel tests to determine the dynamic characteristics of hingeless rotors with hub moment feedb...
The forces and moments at the rotor hub of an Aerospatiale SA349/2 helicopter were investigated. The...
The results are presented of a test program and analysis to investigate the effects of inplane hub s...
Flight tests have been conducted with a medium-size single-rotor helicopter, one blade of which was ...
A full-scale BO-105 hingeless rotor system was tested in the NASA Ames 40- by 80-Foot Wind Tunnel on...
The present report is a study of the dynamic stability of a helicopter with hinged rotor blades unde...
Data from 23 flight conditions, including level flights ranging from advance ratio mu = 0.14 to 0.37...
Flight tests on hingeless rotor compound helicopter to determine level flight and maneuvering charac...
Flight test and analysis of structural loads in helicopter hingeless rotor syste
Flight investigation of control qualities of rudimentary hingeless rotor helicopte
Flight tests have been conducted with a single-rotor helicopter, one blade of which was equipped at ...
A two-blade rotor having a diameter of 4 feet and a solidity of 0.037 was tested in the Langley 300-...
The source of an appreciable pitching-moment difference between left and right hovering turns for a ...
Flight investigations of wing-rotor lift-sharing characteristics of XH-51 helicopte
A study was conducted in which available airload and blade response data for the NH-3A and CH-53A ro...
Wind tunnel tests to determine the dynamic characteristics of hingeless rotors with hub moment feedb...
The forces and moments at the rotor hub of an Aerospatiale SA349/2 helicopter were investigated. The...
The results are presented of a test program and analysis to investigate the effects of inplane hub s...
Flight tests have been conducted with a medium-size single-rotor helicopter, one blade of which was ...
A full-scale BO-105 hingeless rotor system was tested in the NASA Ames 40- by 80-Foot Wind Tunnel on...
The present report is a study of the dynamic stability of a helicopter with hinged rotor blades unde...
Data from 23 flight conditions, including level flights ranging from advance ratio mu = 0.14 to 0.37...