journal article·2000-02

Implications of engine's deterioration upon an aero-engine HP turbine blade's thermal fatigue life

M Naeem

International Journal of Fatigue· Volume 22· Issue 2
Publisher page

Abstract

Possessing a better knowledge of the impacts of engine deterioration upon an aircraft's performance as well as its fuel and component life usage, helps the users make wiser management decisions and hence achieve improved engine utilization. For a military aircraft, using a computer performance simulation, the consequences of engine deterioration on a high pressure turbine blade's thermal fatigue life are predicted.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Fatigue and fracture mechanics · High Temperature Alloys and Creep · Turbomachinery Performance and Optimization

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References

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