Add to ORKGAn axial flow compressor rotor was tested at design speed with six different casing treatments acros...
Strain gages were used to measure blade vibrations possibly causing failure in the 10-stage compress...
International audienceThe use of dynamic seals to reduce the rotor/stator dynamic clearance in jet e...
Friction and fretting wear tests on materials used as friction dampers to reduce vibrational stresse...
Rotor blade aerodynamic damping is experimentally determined in a three-stage transonic axial flow c...
Frequency evaluation in rotary engine blade design is an important research area because of its crit...
PaperPg. 23-34.High blade stresses can be induced in axial compressors by various asymmetrical flow ...
The vibration of a turbocharger blade and dynamic characteristics of bladed packets connected by a l...
The high-cycle fatigue of compressors significantly impacts the lifetime of aircraft engines. Excita...
Turbomachinery blades are subject to aerodynamic forces that can lead to high-cycle-fatigue (HCF) fa...
The compressor case of a 13-stage axial-flow compressor was modified to incorporate air-bleed system...
The importance of blade design parameters in rotor vibratory response and the design of a minimum vi...
February 1981Includes bibliographical references (page 80)A method has been developed and demonstrat...
The overall and blade-element performance of two configurations of a moderately high aspect ratio tr...
This experiment was conducted to measure transverse vibrations of the blades in a transonic compres...
An axial flow compressor rotor was tested at design speed with six different casing treatments acros...
Strain gages were used to measure blade vibrations possibly causing failure in the 10-stage compress...
International audienceThe use of dynamic seals to reduce the rotor/stator dynamic clearance in jet e...
Friction and fretting wear tests on materials used as friction dampers to reduce vibrational stresse...
Rotor blade aerodynamic damping is experimentally determined in a three-stage transonic axial flow c...
Frequency evaluation in rotary engine blade design is an important research area because of its crit...
PaperPg. 23-34.High blade stresses can be induced in axial compressors by various asymmetrical flow ...
The vibration of a turbocharger blade and dynamic characteristics of bladed packets connected by a l...
The high-cycle fatigue of compressors significantly impacts the lifetime of aircraft engines. Excita...
Turbomachinery blades are subject to aerodynamic forces that can lead to high-cycle-fatigue (HCF) fa...
The compressor case of a 13-stage axial-flow compressor was modified to incorporate air-bleed system...
The importance of blade design parameters in rotor vibratory response and the design of a minimum vi...
February 1981Includes bibliographical references (page 80)A method has been developed and demonstrat...
The overall and blade-element performance of two configurations of a moderately high aspect ratio tr...
This experiment was conducted to measure transverse vibrations of the blades in a transonic compres...
An axial flow compressor rotor was tested at design speed with six different casing treatments acros...
Strain gages were used to measure blade vibrations possibly causing failure in the 10-stage compress...
International audienceThe use of dynamic seals to reduce the rotor/stator dynamic clearance in jet e...