TY  - GEN
N2  - This book discusses complex loadings of turbine blades and protective layer Thermal Barrier Coating (TBC), under real working airplane jet conditions. They obey both multi-axial mechanical loading and sudden temperature variation during starting and landing of the airplanes. In particular, two types of blades are analyzed: stationary and rotating, which are widely applied in turbine engines produced by airplane factories.
DO  - 10.1007/978-981-10-0919-8
DO  - doi
AB  - This book discusses complex loadings of turbine blades and protective layer Thermal Barrier Coating (TBC), under real working airplane jet conditions. They obey both multi-axial mechanical loading and sudden temperature variation during starting and landing of the airplanes. In particular, two types of blades are analyzed: stationary and rotating, which are widely applied in turbine engines produced by airplane factories.
T1  - Loadings in thermal barrier coatings of jet engine turbine bladesan experimental research and numerical modeling /
AU  - Sadowski, Tomasz,
AU  - Golewski, Przemysław,
CN  - TA418.76
ID  - 754859
KW  - Thermal barrier coatings.
KW  - Aircraft gas-turbines
SN  - 9789811009198
SN  - 9811009198
TI  - Loadings in thermal barrier coatings of jet engine turbine bladesan experimental research and numerical modeling /
LK  - https://univsouthin.idm.oclc.org/login?url=http://link.springer.com/10.1007/978-981-10-0919-8
UR  - https://univsouthin.idm.oclc.org/login?url=http://link.springer.com/10.1007/978-981-10-0919-8
ER  -