Add to ORKGFriction and fretting wear tests on materials used as friction dampers to reduce vibrational stresses in compressor blades for turbine engine
In jet engines the blade resonant vibration amplitude is normally reduced by increasing the structur...
Fretting fatigue is most likely to occur in the dovetail joint of aero engine compressor resulting i...
The rub mechanics of compressor abradable blade tip seals at simulated engine conditions were invest...
Stress analysis and wear tests in use of lacing wire as vibration damper on turbocompressor blade
High cycle fatigue in blades is triggered by oscillating forces. Devices such as shrouds, that expl...
Bladed disk vibrations in turbomachinery can lead to failure due to High Cycle Fatigue. One way in w...
Nowadays, the increasing demand on the high efficiency energy, low fuel consumption and environment ...
The high-cycle fatigue of compressors significantly impacts the lifetime of aircraft engines. Excita...
The thesis project is directly concerned with safety and reliability as it addresses the problem of ...
The problem of fretting in aircraft turbine engines is discussed. Critical fretting can occur on fan...
The structural damping is of importance to suppress the vibration amplitude of compressor blades rot...
Safety and reliability are two foremost concerns in the design of high-speed rotating equipment. In ...
A lumped parameter method, implemented on a VAX 11/780 computer shows that the primary parameters af...
Turbomachinery blades are subject to aerodynamic forces that can lead to high-cycle-fatigue (HCF) fa...
Engine failures due to fatigue have cost the Air Force an estimated $400 million dollars per year ov...
In jet engines the blade resonant vibration amplitude is normally reduced by increasing the structur...
Fretting fatigue is most likely to occur in the dovetail joint of aero engine compressor resulting i...
The rub mechanics of compressor abradable blade tip seals at simulated engine conditions were invest...
Stress analysis and wear tests in use of lacing wire as vibration damper on turbocompressor blade
High cycle fatigue in blades is triggered by oscillating forces. Devices such as shrouds, that expl...
Bladed disk vibrations in turbomachinery can lead to failure due to High Cycle Fatigue. One way in w...
Nowadays, the increasing demand on the high efficiency energy, low fuel consumption and environment ...
The high-cycle fatigue of compressors significantly impacts the lifetime of aircraft engines. Excita...
The thesis project is directly concerned with safety and reliability as it addresses the problem of ...
The problem of fretting in aircraft turbine engines is discussed. Critical fretting can occur on fan...
The structural damping is of importance to suppress the vibration amplitude of compressor blades rot...
Safety and reliability are two foremost concerns in the design of high-speed rotating equipment. In ...
A lumped parameter method, implemented on a VAX 11/780 computer shows that the primary parameters af...
Turbomachinery blades are subject to aerodynamic forces that can lead to high-cycle-fatigue (HCF) fa...
Engine failures due to fatigue have cost the Air Force an estimated $400 million dollars per year ov...
In jet engines the blade resonant vibration amplitude is normally reduced by increasing the structur...
Fretting fatigue is most likely to occur in the dovetail joint of aero engine compressor resulting i...
The rub mechanics of compressor abradable blade tip seals at simulated engine conditions were invest...