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

Authors
Naeem, M Singh, R Probert, D
Citation
M. Naeem et al., Implications of engine's deterioration upon an aero-engine HP turbine blade's thermal fatigue life, INT J FATIG, 22(2), 2000, pp. 147-160
Citations number
22
Categorie Soggetti
Material Science & Engineering
Journal title
INTERNATIONAL JOURNAL OF FATIGUE
ISSN journal
01421123 → ACNP
Volume
22
Issue
2
Year of publication
2000
Pages
147 - 160
Database
ISI
SICI code
0142-1123(200002)22:2<147:IOEDUA>2.0.ZU;2-K
Abstract
Possessing a better knowledge of the impacts of engine deterioration upon a n aircraft's performance as well as its fuel and component life usage, help s the users make wiser management decisions and hence achieve improved engi ne utilization. For a military aircraft, using a computer performance simul ation, the consequences of engine deterioration on a high pressure turbine blade's thermal fatigue life are predicted. (C) 2000 Elsevier Science Ltd. All rights reserved.