Life prediction in high temperature environments: Overview of a current gas turbine engine approach-Reference-Cited by-同舟云学术

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Life prediction in high temperature environments: Overview of a current gas turbine engine approach

Published:1988-08 Issue:1 Volume:103 Page:63-69
ISSN:0921-5093
Container-title:Materials Science and Engineering: A
language:en
Short-container-title:Materials Science and Engineering: A

Author:

Cowles B.A.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science

Reference23 articles.

1. Cyclic behavior of turbine disk alloys at 650 °C;Cowles;J. Eng. Mater. Technol.,1980

2. Evaluation of the cyclic behavior of aircraft turbine disk alloys — part II;Cowles,1980

3. Engine component retirement for cause: executive summary;Harris,1987

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1. Modeling crack growth of an aircraft engine high pressure compressor blade under combined HCF and LCF loading;Engineering Fracture Mechanics;2019-06

2. A new paradigm of fatigue variability behavior and implications for life prediction;Materials Science and Engineering: A;2007-11

3. Demonstration of advanced life-prediction and state-awareness technologies necessary for prognosis of turbine engine disks;SPIE Proceedings;2004-07-21

4. A microstructure-based fatigue-crack-initiation model;Metallurgical and Materials Transactions A;2003-01

5. High cycle fatigue in aircraft gas turbines—an industry perspective;International Journal of Fracture;1996-04

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