TY  - JOUR
AU  - Silveira, E.
AU  - Atxaga, G.
AU  - Irisarri, A. M.
PY  - 2010
DO  - 10.1016/j.engfailanal.2008.10.015
SN  - 1350-6307
UR  - https://hdl.handle.net/11556/3199
AB  - This paper describes the methodology employed for the failure analysis of aircraft blades and its application to two premature failed sets. The first one corresponds to the high pressure compressor manufactured in a 718 nickel base superalloy. The...
LA  - eng
TI  - Failure analysis of two sets of aircraft blades
TY  - journal article
ER  -