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pro vyhledávání: '"Carol E. Bryant"'
Autor:
Carol E. Bryant, James L. Rutledge
Publikováno v:
Journal of Turbomachinery. 145
High-temperature materials such as ceramic matrix composites (CMCs) are promising for advancements in gas turbine engines; however, experimental techniques are necessary to characterize the thermal behavior of high-temperature materials in scaled rep
Publikováno v:
Journal of Thermophysics and Heat Transfer. 35:644-649
Publikováno v:
Volume 6B: Heat Transfer — General Interest/Additive Manufacturing Impacts on Heat Transfer; Internal Air Systems; Internal Cooling.
An increasingly common experimental technique allows measurement of overall effectiveness by matching the Biot number between experimental and engine conditions. The measured overall effectiveness distribution correlates to the actual turbine compone
Autor:
Carol E. Bryant, James L. Rutledge
Publikováno v:
Volume 6A: Heat Transfer — Combustors; Film Cooling.
An increasingly common experimental technique allows measurement of overall effectiveness by matching the Biot number between experimental and engine conditions. The measured overall effectiveness distribution correlates to the expected turbine compo
Publikováno v:
Journal of Thermal Science and Engineering Applications. 14
In typical film cooling experiments, the adiabatic wall temperature may be determined from surface temperature measurements on a low thermal conductivity model in a low-temperature wind tunnel. In such experiments, it is generally accepted that the a
Autor:
Carol E. Bryant, James L. Rutledge
Publikováno v:
Journal of Thermal Science and Engineering Applications. 14
Increasing interest in the use of ceramic matrix composites (CMCs) for gas turbine engine hot gas path components requires a thorough examination of the thermal behavior one may expect of such components. Their highly anisotropic thermal conductivity
Autor:
Carol E. Bryant, James L. Rutledge
Publikováno v:
Journal of Thermal Science and Engineering Applications. 13
Ceramic matrix composites (CMCs) show promise as higher temperature capable alternatives to traditional metallic components in gas turbine engine hot gas paths. However, CMC components will still require both internal and external cooling, such as fi
Autor:
Carol E. Bryant, James L. Rutledge
Publikováno v:
Journal of Turbomachinery. 142
Gas turbine hot gas path components are protected via coolant that travels through internal passageways before being ejected as external film cooling. Modern computational approaches facilitate simulation of the conjugate heat transfer that takes pla
Publikováno v:
Journal of Turbomachinery. 140
Testing new turbine cooling schemes at engine conditions becomes increasingly cost prohibitive as the desired gas-path temperatures increase. As a result, the turbine component is simulated in a laboratory with a large-scale model that is sized and c