World developments have led the armed forces of many countries to become mo
re aware of how their increasingly-stringent financial budgets are spent. O
ne major expenditure for military authorities is upon aero-engines. Deterio
ration of an engine generally results in a lower specific thrust and higher
specific fuel-consumption for the same spool speeds and turbine-entry temp
eratures. In order to meet the thrust requirement for the same aircraft's p
erformance, the engines are ran at higher spool speeds and/or turbine-entry
temperatures. This results in greater rates of fuel consumption, and a sho
rter life (due to the greater creep damage and low-cycle fatigue incurred).
Possessing a better knowledge, of the impacts of engine deterioration on a
n aircraft's operational performance as well as its fuel and residual life-
expectancy, helps the users to improve engine utilization. (C) 1998 Elsevie
r Science Ltd. ALI rights reserved.