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Estimating Inducer Blade Damping in Water with On-Blade Strain MeasurementsThis paper describes the testing, methodology, and results for estimating critical damping ratios of inducer blade structural natural frequencies. A sub-scale inducer water flow test was performed with on-blade strain gauge measurements. Data were acquired in quiescent air and water, and also at several shaft speeds and operating conditions. Two methods were used to provide active excitation to the blades. The first was to impart a mechanical impulse to the inducer shaft and observe the strain gauge response. The second was to install a stator plate upstream of the inducer to create a non-uniform but regular pressure field at the inducer inlet. There are challenges with using either approach, but damping information was extracted using both methods. Results showed that the critical damping ratio for a given blade mode increased from air to quiescent water, and also increased when the inducer was spinning.
Document ID
20200001004
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Mulder, Andrew
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Skelley, Stephen
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
February 20, 2020
Publication Date
December 9, 2019
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
M19-7783
Report Number: M19-7783
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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