TY  - THES
AU  - ZABEEN, SURAIYA
AU  - DESY
TI  - Fatigue Crack Growth in Complex Residual Stress Fields Due to Surface  Treatment and Foreign Object Damage under Simulated Flight Cycles
PB  - The University of Manchester
VL  - Dissertation
CY  - Manchester
M1  - PHPPUBDB-21609
SP  - 230
PY  - 2011
N1  - Dissertation, The University of Manchester, 2011
AB  - Foreign object damage (FOD) refers to the damage that generally takes place in aero engine fans and compressor blades, due to the ingestion of hard particles/debris during aeroplane take-off, taxiing, or landing. Such damage can reduce the fatigue life expectancy of the turbine engine components by 50
KW  - Dissertation
LB  - PUB:(DE-HGF)11
UR  - https://bib-pubdb1.desy.de/record/96256
ER  -