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Models in the Design and Validation of Eddy Current Inspection for Cracking in the Shuttle Reaction Control System ThrusterA case study is presented for using models in eddy current NDE design for crack detection in Shuttle Reaction Control System thruster components. Numerical methods were used to address the complex geometry of the part and perform parametric studies of potential transducer designs. Simulations were found to show agreement with experimental results. Accurate representation of the coherent noise associated with the measurement and part geometry was found to be critical to properly evaluate the best probe designs.
Document ID
20080031115
Document Type
Conference Paper
Authors
Aldrin, John C. (Computational Tools, Inc. Gurnee, IL, United States)
Williams, Phillip A. (NASA Langley Research Center Hampton, VA, United States)
Wincheski, Russell (Buzz) A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
July 23, 2008
Subject Category
Space Transportation and Safety
Report/Patent Number
LF99-7873
LF99-6957
Meeting Information
35th Annual Review of Progress in Quantitative Nondestructive Evaluation (QNDE)(Chicago, IL)
Funding Number(s)
WBS: WBS 377816.06.02.03.05
Distribution Limits
Public
Copyright
Public Use Permitted.

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