Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Megan Schaenzer"'
Autor:
Scott Yandt, Mahtab Salehii, Miklos Gerendas, Donna Riedel, Lucas Delaby, Ali Shanian, Mitch Kibsey, Matthew Christopher Innes, Megan Schaenzer, Minh Quan Pham, Benoit Villien, David Backman
Publikováno v:
Journal of Engineering Materials and Technology. 144
A novel patterned-void structure is developed to improve the fatigue life compared with conventional circular cooling holes typically used in gas turbine components exposed to high temperatures. The distinctive S-shape of the voids and their specific
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::22a04f75fc6111434cf154e602009b12
https://doi.org/10.1115/1.4052251
https://doi.org/10.1115/1.4052251
Autor:
Jose L. Rodriguez, Yakym Khlyapov, Erik Fernandez, Husam Zawati, Megan Schaenzer, Gaurav Gupta, Jayanta S. Kapat
Publikováno v:
Volume 7A: Heat Transfer.
The objective of the present study is the evaluation of the heat transfer difference between a novel jet plate configuration and a conventional flat jet orifice plate. Physical mechanisms that lead to a change in Nusselt number when comparing both co
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4f2a961d6b1a5f108c61aa4c30203976
https://doi.org/10.1115/gt2020-16102
https://doi.org/10.1115/gt2020-16102
Autor:
Omar Valero, Li He, Roger Wells, Yan Sheng Li, Gaurav Gupta, Jayanta S. Kapat, Marios Kapsis, Megan Schaenzer, Senthil Krishnababu
Publikováno v:
Journal of Engineering for Gas Turbines and Power. 142
Typical turbomachinery aerothermal problems of practical interest are characterized by flow structures of wide-ranging scales, which interact with each other. Such multiscale interactions can be observed between the flow structures produced by surfac
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::75c7f23f38507853b31b08b5d65d5478
https://doi.org/10.1115/1.4045481
https://doi.org/10.1115/1.4045481
Autor:
Minh Quan Pham, Thomas Scarinci, Scott Yandt, Christopher Booth-Morrison, Katia Bertoldi, Matthew Christopher Innes, Ahmad Rafsanjani, Farhad Javid, Megan Schaenzer, Ali Shanian, Jia Liu, Miklos Gerendas, David Backman
Publikováno v:
Extreme Mechanics Letters. 16:13-17
Many components of gas turbines, including the combustion liners, ducts, casings and sealing structures, comprise metallic sheets perforated with arrays of circular cooling holes. These parts are highly prone to fatigue failure due to the stresses in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::92a78bc172e7b40002d94f3e38799142
https://doi.org/10.1016/j.eml.2017.08.002
https://doi.org/10.1016/j.eml.2017.08.002
Autor:
Megan Schaenzer, Senthil Krishnababu, Gaurav Gupta, Roger Wells, Marios Kapsis, Omar Valero, Li He, Jayanta S. Kapat, Yan Sheng Li
Publikováno v:
Volume 2C: Turbomachinery.
Typical turbomachinery aerothermal problems of practical interest are characterised by flow structures of wide-ranging scales, which interact with each other. Such multi-scale interactions can be observed between the flow structures produced by surfa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7bd2cdcbbe8b7a2b4dd1d1507583e0df
https://doi.org/10.1115/gt2019-90314
https://doi.org/10.1115/gt2019-90314
Autor:
Jiazhen Leng, Aziz Madrane, Damiano Pasini, Minh Quan Pham, Ali Shanian, Megan Schaenzer, Genevieve Bourgeois, Haichao An
Publikováno v:
International Journal of Thermal Sciences. 158:106542
This paper presents a gradient-based framework to optimize the film-cooling performance of heat bearing components in gas turbines. We examine a representative periodic component with very low porosity (below 1 % ) and optimize the shape of an inclin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8e88864f8173d236e820403dee73cfdc
https://doi.org/10.1016/j.ijthermalsci.2020.106542
https://doi.org/10.1016/j.ijthermalsci.2020.106542
Publikováno v:
Smart Materials and Structures. 29:125004
Gas turbine blades are subjected to unusually harsh operating conditions—rotating at high velocities in gas streams whose temperature can exceed the melting temperature of the blade. In order to survive these conditions, the blade must efficiently
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::25fe28190439e0cb79189d9e27824c8c
https://doi.org/10.1088/1361-665x/abbd1d
https://doi.org/10.1088/1361-665x/abbd1d
Autor:
Ali Shanian, Megan Schaenzer, Genevieve Bourgeois, Mehran Farhangi, Minh Quan Pham, François-Xavier Jette, Matt Innes, Fabian Sanchez
Publikováno v:
Volume 4A: Combustion, Fuels, and Emissions.
Cooling holes in combustion liners are typically circular, as are the holes used for acoustic damping of combustor instabilities. This hole geometry is chosen for several reasons, which include manufacturability, stress concentration considerations,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0cc51dc1ed7e7ebed9b84a608b316a52
https://doi.org/10.1115/gt2018-75837
https://doi.org/10.1115/gt2018-75837
Autor:
Farhad Javid, Ali Shanian, Mahtab Salehii, Tobias Meis, Dieter Peitsch, Scott Yandt, Friedrich Bake, François-Xavier Jette, Miklos Gerendas, David Backman, Andrew J. Gross, Karsten Knobloch, Katia Bertoldi, Minh Quan Pham, Megan Schaenzer, Genevieve Bourgeois
Publikováno v:
Advanced Engineering Materials. 21:1900084
Mechanical metamaterials have attracted great interest due their ability to attain material properties outside the bounds of those found in natural materials. Many promising mechanical metamaterials have been designed, fabricated, and tested, however
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0eb5e7d80b10251fd93e7ed9f79f1181
https://doi.org/10.1002/adem.201900084
https://doi.org/10.1002/adem.201900084