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A Unique, Rapid Uncertainty Analysis for Turbine Engine Testing FREE

[+] Author Affiliations
Christopher A. Boedicker

AF Wright Aeronautical Laboratories, Wright-Patterson AFB, OH

Paper No. 86-GT-280, pp. V002T02A019; 7 pages
doi:10.1115/86-GT-280
From:
  • ASME 1986 International Gas Turbine Conference and Exhibit
  • Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery
  • Dusseldorf, West Germany, June 8–12, 1986
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7929-0
  • Copyright © 1986 by ASME

abstract

I have developed and implemented a computer subroutine (UNCERT) that greatly simplifies the immense problems associated with most uncertainty analyses. This paper presents an overview of the most fundamental and important concepts in uncertainty analysis, a technique which can be used by a test engineer to estimate the accuracy of measured data and values calculated from measured data. Implementation of these uncertainty concepts in a computer code is also explained. Some of the results of an uncertainty analysis which was accomplished for a turbine engine compressor test are used to illustrate the analysis procedure and results. Finally, the benefits of doing an uncertainty analysis as part of a test are briefly discussed.

Copyright © 1986 by ASME
This article is only available in the PDF format.

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