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Biopolymers in Nanocoating: Principles and Applications. [PDF]
Bharathi VSK, Jayas DS.
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Progress in Materials for Metallic Cultural Heritage Conservation: Mechanisms, Applications, and Future Perspectives. [PDF]
Liu Y, Liu X, Xu S, Liu X.
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Review of Recent Advances in Cold-Sprayed Coatings for Accident-Tolerant Fuel Cladding. [PDF]
Mou Y +10 more
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A Comprehensive Review of Zero-Dimensional Carbon-Based Nanomaterials in Anti-Corrosive Coating Applications: A Combined Quantitative and Qualitative Analysis. [PDF]
Liu X +6 more
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Sustainable Functional Polymer Composites: Bio-Based Systems with Tailored Properties for Civil Engineering Applications-A Review. [PDF]
Iftikhar A, Manalo A, Peerzada M.
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Nanocellulose Materials: Processing, Properties, and Application. [PDF]
Burchett A +6 more
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Le Journal de Physique IV, 2001
The use of Thermal Barrier Coatings (=TBC) in gas turbines allows to increase the working temperature and therefore the yield of gas turbines. Conventional TBC's (Y 2 O 3 -stabilised ZrO 2 ) are produced by plasma spraying and , electron beam evaporation. CVD processes for the production of TBC's are under investigation.
G. Wahl, Ch. Metz, S. Samoilenkov
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The use of Thermal Barrier Coatings (=TBC) in gas turbines allows to increase the working temperature and therefore the yield of gas turbines. Conventional TBC's (Y 2 O 3 -stabilised ZrO 2 ) are produced by plasma spraying and , electron beam evaporation. CVD processes for the production of TBC's are under investigation.
G. Wahl, Ch. Metz, S. Samoilenkov
openaire +2 more sources
Journal of Thermal Spray Technology, 1996
The fundamental driving force for the development of thermal barrier coatings has been the continuing quest for ever higher temperatures in gas turbines. Over the period 1940–1970, the temperature capability of superalloys for gas turbine blades, which is defined in terms of 100 h life at 20000 psi (138 MPa) stress, was increased from approximately ...
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The fundamental driving force for the development of thermal barrier coatings has been the continuing quest for ever higher temperatures in gas turbines. Over the period 1940–1970, the temperature capability of superalloys for gas turbine blades, which is defined in terms of 100 h life at 20000 psi (138 MPa) stress, was increased from approximately ...
openaire +2 more sources
Thermal Conductivity of a Zirconia Thermal Barrier Coating
Journal of Thermal Spray Technology, 1998The conductivity of a thermal-barrier coating composed of atmospheric plasma sprayed 8 mass percent yttria partially stabilized zirconia has been measured. This coating was sprayed on a substrate of 410 stainless steel. An absolute, steady-state measurement method was used to measure thermal conductivity from 400 to 800 K.
Slifka, Andrew J. +4 more
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