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Determination of Appropriate Multiple K of Damping Standard Deviation for Use in Calculation of Turbine Blade Forced ResponseNo abstract available
Document ID
20150021446
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Brown, Andy (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
November 19, 2015
Publication Date
September 1, 2015
Subject Category
Structural Mechanics
Aircraft Propulsion And Power
Report/Patent Number
M16-4915
Meeting Information
Meeting: GUIde 5 Annual Meeting
Location: Indianapolis, IN
Country: United States
Start Date: October 23, 2015
Sponsors: Duke Univ.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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