Methods developed for measuring blade and rotor-shaft system response include optical systems, transient instruments, and special digital data processing equipment. Optical methods offer some distinct benefits for blade vibration measurement. Transient and steady state measurements of the response of rotor-shaft systems strongly affect analytical methods development. Digital computing systems allow processing of large volumes of high speed data from rotating blade sets. Also, digital systems develop useful vibration response signatures from randomly excited systems. Research facilities include the spin rig facility and the transient rotor response lab
The NASA Lewis Research Center has developed and implemented a time-efficient methodology for dynami...
Although noninterference optical instrumentation has been previously used to monitor and measure rot...
The purpose of this report is to provide a description of the overall thrust, past relevant accompli...
A new concept in instrumentation was developed by engineers at NASA Lewis Research Center to collect...
The need for a structural dynamics verification facility to support structures programs was studied....
A system for turbo machinery blade vibration has been developed that combines time-of-arrival sensor...
The Lewis Research Center spin rig was constructed to provide experimental evaluation of analysis me...
In the noninterference measurement of blade vibrations, a laser light beam is transmitted to the rot...
Gas turbine engines are currently being designed to have increased performance, lower weight and man...
NASA Lewis Research Center's Dynamic Spin Rig, located in Building 5, Test Cell CW-18, is used to te...
A low cost optical data acquisition system was designed to measure deflection of vibrating rotor bla...
All turbomachinery blades experience vibration under operating conditions. Given that theoretical to...
The Dynamic Spin Rig Facility at the NASA Glenn Research Center is used to determine the structural ...
The Dynamic Spin Rig (DSR) is used to perform vibration tests of turbomachinery blades and component...
An overview of the methods and concepts developed to enhance and predict structural dynamic characte...
The NASA Lewis Research Center has developed and implemented a time-efficient methodology for dynami...
Although noninterference optical instrumentation has been previously used to monitor and measure rot...
The purpose of this report is to provide a description of the overall thrust, past relevant accompli...
A new concept in instrumentation was developed by engineers at NASA Lewis Research Center to collect...
The need for a structural dynamics verification facility to support structures programs was studied....
A system for turbo machinery blade vibration has been developed that combines time-of-arrival sensor...
The Lewis Research Center spin rig was constructed to provide experimental evaluation of analysis me...
In the noninterference measurement of blade vibrations, a laser light beam is transmitted to the rot...
Gas turbine engines are currently being designed to have increased performance, lower weight and man...
NASA Lewis Research Center's Dynamic Spin Rig, located in Building 5, Test Cell CW-18, is used to te...
A low cost optical data acquisition system was designed to measure deflection of vibrating rotor bla...
All turbomachinery blades experience vibration under operating conditions. Given that theoretical to...
The Dynamic Spin Rig Facility at the NASA Glenn Research Center is used to determine the structural ...
The Dynamic Spin Rig (DSR) is used to perform vibration tests of turbomachinery blades and component...
An overview of the methods and concepts developed to enhance and predict structural dynamic characte...
The NASA Lewis Research Center has developed and implemented a time-efficient methodology for dynami...
Although noninterference optical instrumentation has been previously used to monitor and measure rot...
The purpose of this report is to provide a description of the overall thrust, past relevant accompli...