Add to ORKGThe research accomplished in the area of rotor loads over the last 13 to 14 years is reviewed. The s...
Research is presented on helicopter rotor blade vibration and on two and three dimensional analyses ...
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...
The problems that were encountered in the dynamics of advanced rotor systems are described. The meth...
The requirement for low vibrations has achieved the status of a critical design consideration in mod...
Excessive vibration remains one one of the most difficult problems that faces the helicopter industr...
Theoretical and experimental developments in the aeroelastic and aeromechanical stability of helicop...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76177/1/AIAA-9022-592.pd
Helicopter airframe vibration is examined using calculations and measurements for the SA349/2 resear...
The rotor dynamic design considerations are essentially limitations on the vibratory response of the...
Issued as Reports [nos. 1-2], Monthly reports [nos. 1-5], Progress reports [nos. 1-2], and Final rep...
Over fifty years of contributions by NASA and the Army through rotor systems flight research were ex...
In the conference proceedings are 24 presented papers, their discussions, and material given in two ...
Highlights of nine different research studies are described. Five of these topics relate directly to...
The research accomplished in the area of rotor loads over the last 13 to 14 years is reviewed. The s...
Research is presented on helicopter rotor blade vibration and on two and three dimensional analyses ...
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...
The problems that were encountered in the dynamics of advanced rotor systems are described. The meth...
The requirement for low vibrations has achieved the status of a critical design consideration in mod...
Excessive vibration remains one one of the most difficult problems that faces the helicopter industr...
Theoretical and experimental developments in the aeroelastic and aeromechanical stability of helicop...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76177/1/AIAA-9022-592.pd
Helicopter airframe vibration is examined using calculations and measurements for the SA349/2 resear...
The rotor dynamic design considerations are essentially limitations on the vibratory response of the...
Issued as Reports [nos. 1-2], Monthly reports [nos. 1-5], Progress reports [nos. 1-2], and Final rep...
Over fifty years of contributions by NASA and the Army through rotor systems flight research were ex...
In the conference proceedings are 24 presented papers, their discussions, and material given in two ...
Highlights of nine different research studies are described. Five of these topics relate directly to...
The research accomplished in the area of rotor loads over the last 13 to 14 years is reviewed. The s...
Research is presented on helicopter rotor blade vibration and on two and three dimensional analyses ...
The use of a computer program for a comprehensive analytical model of rotorcraft aerodynamics and dy...