Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Randall Mathison"'
Publikováno v:
Journal of Engineering for Gas Turbines and Power. 145
As improved efficiency goals require ever smaller gaps between rotating turbomachinery blade tips and stationary outer casings, it becomes more important to understand the physics of what happens when a blade tip rubs against the casing. A key piece
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ab1912d0e4f9769e5bbd3bf086b13495
https://doi.org/10.1115/1.4055884
https://doi.org/10.1115/1.4055884
Publikováno v:
Volume 6B: Heat Transfer — General Interest/Additive Manufacturing Impacts on Heat Transfer; Internal Air Systems; Internal Cooling.
Unsteady flow fields are generated in gas turbines due to interactions between rotating and stationary components. Increased understanding of unsteadiness and its effect on blade heat transfer is crucial to thermal durability predictions for turbine
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7ddf5bbebeb37d2c58de9043f2df5d33
https://doi.org/10.1115/gt2022-78272
https://doi.org/10.1115/gt2022-78272
Publikováno v:
Volume 6A: Heat Transfer — Combustors; Film Cooling.
Gas turbines generate highly unsteady flow fields, which are further complicated by cooling. Film cooling technology is dependent on experimental and computational research performed for simplified geometries, which can be difficult to translate to t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e2b41efb123df938e908405f061dfb68
https://doi.org/10.1115/gt2022-78244
https://doi.org/10.1115/gt2022-78244
Publikováno v:
Volume 6A: Heat Transfer — Combustors; Film Cooling.
To provide a detailed analysis of film cooling in a turbine environment, this study incorporates experimental and computational research performed on a rotating high pressure turbine stage. The turbine blades include rows of three different film cool
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c4035d29d1db6f35b4ca5c2026533608
https://doi.org/10.1115/gt2022-78245
https://doi.org/10.1115/gt2022-78245
Publikováno v:
Volume 6B: Heat Transfer — General Interest/Additive Manufacturing Impacts on Heat Transfer; Internal Air Systems; Internal Cooling.
Axial gas turbines set up highly complex unsteady flow fields, and the incorporation of cooling further complicates the flow. Due to time and computational resource constraints, the design cycle for modern gas turbines relies heavily on steady-state
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::810a934ae39f708956577c5299b134f7
https://doi.org/10.1115/gt2022-78273
https://doi.org/10.1115/gt2022-78273
Publikováno v:
Volume 8B: Structures and Dynamics — Probabilistic Methods; Rotordynamics; Structural Mechanics and Vibration.
As improved efficiency goals require ever smaller gaps between rotating turbomachinery blade tips and stationary outer casings, it becomes more important to understand the physics of what happens when a blade tip rubs against the casing. A key piece
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::018ee31e5c4fbea263d3ccfe42fec0d7
https://doi.org/10.1115/gt2022-83344
https://doi.org/10.1115/gt2022-83344
Publikováno v:
Volume 6B: Heat Transfer — General Interest/Additive Manufacturing Impacts on Heat Transfer; Internal Air Systems; Internal Cooling.
Flow fields in axial gas turbines are highly complex and unsteady due to the interactions of rotating and stationary components. The current study incorporates experimental and computational analyses of a modern, rotating high-pressure turbine stage
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d322bef6209ad4008709db7b59d5865b
https://doi.org/10.1115/gt2022-78271
https://doi.org/10.1115/gt2022-78271
Publikováno v:
Journal of Turbomachinery. 139
Cooling flow behavior is investigated within the multiple serpentine passages with turbulators on the leading and trailing walls of an axial gas turbine blade operating at design-corrected conditions with accurate external flow conditions. Pressure a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f7a1d8f43db63d95afe63fc889623246
https://doi.org/10.1115/1.4036109
https://doi.org/10.1115/1.4036109