%0 Thesis
%A ZABEEN, SURAIYA
%A DESY
%T Fatigue Crack Growth in Complex Residual Stress Fields Due to Surface  Treatment and Foreign Object Damage under Simulated Flight Cycles
%I The University of Manchester
%V Dissertation
%C Manchester
%M PHPPUBDB-21609
%P 230
%D 2011
%Z Dissertation, The University of Manchester, 2011
%X 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
%K Dissertation
%F PUB:(DE-HGF)11
%9 Dissertation / PhD Thesis
%U https://bib-pubdb1.desy.de/record/96256