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Scaling Techniques for Combustion Device Random Vibration PredictionsThis work presents compares scaling techniques that can be used for prediction of combustion device component random vibration levels with excitation due to the internal combustion dynamics. Acceleration and unsteady dynamic pressure data from multiple component test programs are compared and normalized per the two scaling approaches reviewed. Two scaling technique are reviewed and compared against the collected component test data. The first technique is an existing approach developed by Barrett, and the second technique is an updated approach new to this work. Results from utilizing both techniques are presented and recommendations about future component random vibration prediction approaches are given.
Document ID
20170000438
Acquisition Source
Marshall Space Flight Center
Document Type
Abstract
Authors
Kenny, R. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Ferebee, R. C.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Duvall, L. D.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
January 13, 2017
Publication Date
December 5, 2016
Subject Category
Acoustics
Structural Mechanics
Report/Patent Number
M16-5406
Meeting Information
Meeting: JANNAF Liquid Propulsion (LPS) meeting
Location: Phoenix, AZ
Country: United States
Start Date: December 5, 2016
End Date: December 8, 2016
Sponsors: NASA Headquarters, Department of the Army, Department of the Navy, Department of the Air Force
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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