Numerical study for life prediction and optimization of advanced thermal barrier coatings

논문상세정보
' Numerical study for life prediction and optimization of advanced thermal barrier coatings' 의 주제별 논문영향력
논문영향력 선정 방법
논문영향력 요약
주제
  • Finite element method
  • Thermal barrier coatings
  • doubleceramiclayer
  • life prediction
  • rare-earthelement
동일주제 총논문수 논문피인용 총횟수 주제별 논문영향력의 평균
173 0

0.0%

' Numerical study for life prediction and optimization of advanced thermal barrier coatings' 의 참고문헌

  • cerium oxide as a thermal barrier-coating material for high-temperature applications
    [2003]
  • accurate high temperature engine aerothermal measurements for gas-turbine life optimisation , performance and condition monitoring )
    [2010]
  • [8] Eung Sun Byon. Thermal barrierCoatings for gas turbine engineComponents. Korea Institute of Materials Science News, 17(4):34?38, 2014.
    17 ( 4 ) :34 ? 38 [2014]
  • [51] Tomasz Sadowski and Przemyslaw Golewski. Loadings in thermal barrier coatings of jet engine turbine blades: An experimental research and numerical modeling. Springer, 2016.
  • [35] Marcin Bia las. Finite element analysis of stress distribution in thermal barrierCoatings. Surface andCoatings Technology, 202(24):6002?6010, 2008.
    [2008]
  • [19] FH Stott and GC Wood. Growth and adhesion of oxide scales on al2o3-forming alloys andCoatings. Materials Science and Engineering, 87:267?274, 1987.
    274 [1987]
  • Zirconates as new materials for thermal barrier coatings
    83 ( 8 ) :2023 ? 2028 [2000]
  • Yb2o3 and gd2o3 doped strontium zirconate for thermal barrier coatings
    28 ( 16 ) :3071 ? 3081 [2008]
  • Vapor deposited samarium zirconate thermal barrier coatings . Surface and Coatings Technology , 203 ( 20-21 ) :3157 ? 3167
    [2009]
  • Turbine cooling and heat transfer modelling for gas turbine performance simulation
    [2015]
  • Thermal-barrier coatings for more efficient gas-turbine engines
    37 ( 10 ) :891 ? 898 [2012]
  • Thermal shock resistance and mechanical properties of la2ce2o7 thermal barrier coatings with segmented structure
    [2009]
  • Thermal cycling behavior of la2ce2o7/8ysz double-ceramic-layer thermal barrier coatings prepared by atmospheric plasma spraying .
    [2010]
  • Thermal barrier coatings technology : critical review , progress update , remaining challenges and prospects
    58 ( 6 ) :315 ? 348 [2013]
  • Thermal barrier coatings for turbine airfoils . Thin Solid Films , 127 ( 1-2 ) :93 ? 106
    [1985]
  • Thermal barrier coatings for gas-turbine engine applications . Science , 296 ( 5566 ) :280 ?
    284 [2002]
  • Thermal barrier coating materials
    8 ( 6 ) :22 ? 29 [2005]
  • Thermal barrier coating life prediction model development
    [1988]
  • The thermal cycling behavior of lanthanum ? cerium oxide thermal barrier coating prepared by eb ? pvd . Surface and Coatings Technology , 200 ( 16-17 ) :5113 ? 5118
    [2006]
  • The feasibility of heat pipe turbine vane cooling . In ASME 1994 International Gas Turbine and Aeroengine Congress and Exposition
    [1994]
  • The evolution of thermal barrier coatings in gas turbine engine applications . In ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition , pages V005T13A001 ? V005T13A001
    [1992]
  • Tensile cracking during thermal cycling of alumina films formed by high-temperature oxidation .
    47 ( 13 ) :3589 ? 3605 [1999]
  • Synthesis kinetics and thermophysical properties of la2 ( zr0 . 7ce0 . 3 ) 2o7 ceramic for thermal barrier coatings . Journal of Rare Earths
    30 ( 3 ) :228 ? 232 [2012]
  • Surfaceroughness induced residual stresses in thermal barrier coatings : computer simulations
    volume 308 , pages 442 ? 449 [1999]
  • Simulation of stresses and delamination in a plasma-sprayed thermal barrier system upon thermalCycling .
    [2003]
  • Segmented lanthanumCerium oxide thermal barrierCoatings by atmospheric plasma spray . Surface Engineering
    25 ( 7 ) :555 ? 558 [2009]
  • ProtectiveCoatings in the gas turbine engine
    9 [1994]
  • Progress in life time modeling of aps-tbc part ii :Critical strains , macro-cracking , and thermal fatigue .
    21 ( 2 ) :77 ? 86 [2004]
  • Predicting failure within tbc system : Finite element simulation of stress within tbc system as affected by sintering of aps tbc , geometry of substrate andCreep of tgo .
    164 [2013]
  • Phase stability of zirconia-based thermal barrier coatings part i. zirconia-yttria alloys
    46 ( 1 ) :75 ? 90 [1991]
  • Particle in-flight behavior and its influence on the microstructure and mechanical property of plasma sprayed la2ce2o7 thermal barrier coatings
    185 [2015]
  • Oxide layer rumpling control technology for high efficiency of eco-friendly combined-cycle power generation system
    7 ( 1 ) :185 ? 193 [2020]
  • Oxidation characteristics of a platinized mcraly bond coat for tbc systems during cyclic oxidation at 1000 c. Surface and coatings technology
    199 ( 1 ) :77 ? 82 [2005]
  • Optimization selection of the thermal conductivity of the top ceramic layer in the double-ceramic-layer thermal barrier coatings based on the finite element analysis of thermal insulation
    326 [2014]
  • Numerical investigation of residual stress fields and crack behavior in tbc systems
    [2002]
  • New thermal barrier coatings based on pyrochlore/ysz double-layer systems
    1 ( 4 ) :351 ? 361 [2004]
  • Modeling of residual stresses in a plasma-sprayed zirconia/alumina functionally graded-thermal barrier coating . Thin Solid Films , 434 ( 1-2 ) :216 ? 227
    [2003]
  • Mechanisms controlling the durability of thermal barrier coatings
    [2001]
  • Mechanical and physical properties of engineering alumina ceramics
    volume 23 [1996]
  • Lifetime of plasma-sprayed thermal barrier coatings : comparison of numerical and experimental results
    18 ( 5-6 ) :835 [2009]
  • Life prediction method for thermal barrier coating of high-efficiency eco-friendly combined cycle power plant
    6 ( 2 ) :329 ? 337 [2019]
  • Life modeling of thermal barrier coatings for aircraft gas turbine engines
    [1988]
  • Lanthanum ? titanium ? aluminum oxide : a novel thermal barrier coating material for applications at 1300 ‘ c. Journal of the European Ceramic Society
    31 ( 9 ) :1677 ? 1683 [2011]
  • Korean Gas Turbine Development and Strategy
    36 [2014]
  • Introduction to the high temperature oxidation of metals
    [2006]
  • Hot corrosion behavior and wettability of calcium ? magnesium ? alumina ? silicate ( cmas ) on lati2al9o19 ceramic
    [2019]
  • High-temperature stress measurements during the oxidation of nial . Oxidation of metals , 53 ( 3-4 ) :259 ? 272
    [2000]
  • Gas turbine technology evolution : A designers perspective . Journal of propulsion and power
    20 ( 4 ) :577 ? 595 [2004]
  • Gas turbine technology
    38 ( 6 ) :504 [2003]
  • Gas turbine heat transfer and cooling technology
    [2012]
  • Fracture toughness measurements of plasma-sprayed thermal barrier coatings using a modified four-point bending method
    204 ( 24 ) :4066 ? 4074 [2010]
  • Finite element simulation of residual stress of double-ceramic-layer la2zr2o7/8ysz thermal barrier coatings using birth and death element technique .
    53 ( 1 ) :117 ? 127 [2012]
  • Failure mechanisms associated with the thermally grown oxide in plasma-sprayed thermal barrier coatings
    [2000]
  • Evaluation of optimal top coat thickness in composite lta/ysz thermal barrier coating by comparative stress distribution using finite element method
    52 ( 4 ) :146 ? 150 [2015]
  • Effect of oxide growth on the stress development in double-ceramic-layer thermal barrier coatings
    [2017]
  • Edge effects in thin film delamination
    49 ( 1 ) :93 ? 107 [2001]
  • Eb-pvd processing of pyrochlorestructured la2zr2o7-based tbcs .
    182 ( 2-3 ) :175 ? 183 [2004]
  • Directions of the development of thermal barrier coatings in energy applications
    202 [1999]
  • Development of a durability evaluation model to optimize rare-earth-element-based thermal barrier coatings
    [2019]
  • Determination of creep behavior of thermal barrier coatings under laser imposed temperature and stress gradients
    [1997]
  • Deformation mechanism maps : the plasticity and creep of metals and ceramics
    [1982]
  • Damage mechanisms and lifetime behavior of plasma-sprayed thermal barrier coating systems for gas turbines ? part ii : Modeling
    [2008]
  • Crystal structure , hydration and ionic conductivity of the inherently oxygendeficient la2ce2o7 .
    7 [2012]
  • Criteria for the delamination of thermal barrier coatings : with application to thermal gradientsSurface and Coatings Technology , 185 ( 2-3 ) :184 ? 193
    [2004]
  • Crack propagation modeling on the interfaces of thermal barrier coating system with different thickness of the oxide layer and different interface morphologies
    32 ( 10 ) :4961 ? 4969 [2011]
  • Comparison of thermal cycling behavior of plasma-sprayed nanostructured and traditional thermal barrier coatings
    [2007]
  • Ceria precipitation and phase stability in zirconia based thermal barrier coatings
    [1995]
  • Assessment of tbc systems failure mechanisms using a fracture mechanics approach
    53 ( 16 ) :4399 ? 4413 [2005]
  • Analytical modeling of oxide thickness effects on residual stresses in thermal barrier coatings
    [2000]
  • A software tool for lifetime prediction of thermal barrier coating systems
    59 ( 7 ) :556 ? 565 [2008]
  • A parametric study of the doubleceramic-layer thermal barrier coating part ii : Optimization selection of mechanical parameters of the inside ceramic layer based on the effect on the stress distribution
    117 [2014]
  • A parametric study of the double-ceramic-layer thermal barrier coatings part i : Optimization design of the ceramic layer thickness ratio based on the finite element analysis of thermal insulation ( take lz7c3/8ysz/nicoaly dcl-tbc for an example )
    509 [2013]
  • A finite element analysis technique for predicting as-sprayed residual stresses generated by the plasma spray coating process
    41 ( 13 ) :1235 ? 1254 [2005]