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020 _a9789811009198
040 _aES-MaUEC
050 4 _aTA418.76
_bS236 2016 EB
082 0 4 _a620.1
100 1 _aSadowski, Tomasz.
_9100880
_0Local
245 1 0 _aLoadings in Thermal Barrier Coatings of Jet Engine Turbine Blades :
_bAn Experimental Research and Numerical Modeling
_cby Tomasz Sadowski, Przemysław Golewski
260 _aSingapore
_bSpringer
_c2016
300 _a1 recurso en línea (VIII, 107 p.) 30 il., 20 il. col.
336 _aTexto (visual)
_btxt
_2rdacontent
337 _aelectrónico
_bc
_2rdamedia
338 _arecurso electrónico
_bcr
_2rdacarrier
338 _aonline resource
_bcr
_2rdacarrier
490 1 _aSpringerBriefs in Applied Sciences and Technology
_x2191-530X
520 _aThis 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.
942 _2lcc
_cLE
988 0 0 _aEBOOK, EBSPRINGER
650 7 _aModelos matemáticos
_0comprobar BNE19900964919
_2embne
_9405064
650 7 _aMecánica de medios continuos
_0comprobar BNE19901010811
_2embne
_9142188
650 0 7 _aIngeniería
_vCongresos y asambleas
_0LocalX
_2embne
_9670301
700 1 _aGolewski, Przemysław
_0Local
_9100881
830 0 _aSpringerBriefs in Applied Sciences and Technology
_x2191-530X
_9134085
856 4 0 _uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://link.springer.com/book/10.1007/978-981-10-0919-8
_zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
901 _ai9789811009198
907 _a.b12961243
_b10-10-17
_c21-11-16
998 _am
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_a_vill
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_z06-04-17
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