Results 141 to 150 of about 55,297 (275)
Emittance and absorptance of NASA ceramic thermal barrier coating system [PDF]
Spectral emittance measurements were made on a two-layer ceramic thermal barrier coating system consisting of a metal substrate, a NiCrAly bond coating and a yttria-stabilized zirconia ceramic coating.
Liebert, C. H.
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Creep of plasma sprayed zirconia [PDF]
Specimens of plasma-sprayed zirconia thermal barrier coatings with three different porosities and different initial particle sizes were deformed in compression at initial loads of 1000, 2000, and 3500 psi and temperatures of 1100 C, 1250 C, and 1400 C ...
Adams, J. W. +2 more
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Thermal barrier coating life-prediction model development [PDF]
Life predictions are made for two types of strain-tolerant and oxidation-resistant Thermal Barrier Coating (TBC) systems produced by commercial coating suppliers to the gas turbine industry.
Neumann, J., Strangman, T. E.
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Compatibility of grain-stabilized platinum with candidate propellants for resistojets [PDF]
Resistojets are candidates for space station auxiliary propulsion, and should be characterized by both long life and multipropellant operations, requirements limited by available materials.
Grisnik, S. P., Whalen, M. V.
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Metal-to-ceramic seals for thermionic converters - A literature survey [PDF]
Metal to ceramic sealing techniques for thermionic converters - literature ...
Phillips, W. M.
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Performance of thermal barrier coatings in high heat flux environments [PDF]
Thermal barrier coatings were exposed to the high temperature and high heat flux produced by a 30 kW plasma torch. Analysis of the specimen heating rates indicates that the temperature drop across the thickness of the 0.038 cm ceramic layer was about ...
Berndt, C. C., Miller, R. A.
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Journal of Aerospace Technology and Management, 2011 The most usual ceramic material for coating turbine blades is yttria doped zirconia. Addition of niobia, as a co-dopant in the Y2O3-ZrO2 system, can reduce the thermal conductivity and improve mechanical properties of the coating.
Daniel Soares de Almeida +3 more
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Ceramic thermal-barrier coatings for cooled turbines [PDF]
Coating systems consisting of a plasma sprayed layer of zirconia stabilized with either yttria, magnesia or calcia over a thin alloy bond coat have been developed, their potential was analyzed and their durability and benefits evaluated in a turbojet ...
Liebert, C. H., Stepka, F. S.
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Feasibility of yttria-stabilized zirconia [PDF]
American Journal of Orthodontics and Dentofacial Orthopedics, 2017 openaire +2 more sources
Development of high temperature materials for solid propellant rocket nozzle applications [PDF]
Aspects of the development and characteristics of thermal shock resistant hafnia ceramic material for use in solid propellant rocket nozzles are presented.
Lineback, L. D., Manning, C. R., Jr.
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