TY  - JOUR
AU  - Mendia, L.
AU  - Estensoro, F. J.
AU  - Mary, C.
AU  - Vogel, F.
PY  - 2011
DO  - 10.1016/j.proeng.2011.04.301
SN  - 1877-7058
UR  - https://hdl.handle.net/11556/3383
AB  - Gas turbine blades are subjected to very high levels of stress and temperature during each engine operating cycle. Superimposed upon this quasy-steady state condition, blades also endure vibrational stresses induced by local perturbations. When...
LA  - eng
TI  - Effect of combined cycle fatigue on Ti6242 fatigue strength
TY  - journal article
ER  -