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Engine Component Life Prediction Methodology for Conceptual Design Investigations FREE

[+] Author Affiliations
John D. Cyrus

Naval Air Development Center

Paper No. 86-GT-24, pp. V002T02A003; 8 pages
doi:10.1115/86-GT-24
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

The increasing emphasis on engine durability requires that an analytical capability be acquired to assess engine component lives during the conceptual/preliminary design phases. A generalized methodology has been developed to provide a fundamental understanding of the impact of engine design decisions, material selections, and a detailed consideration of engine usage for critical gas turbine engine components.

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

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