Zobrazeno 1 - 10
of 34
pro vyhledávání: '"Krishna Venkatesan"'
Publikováno v:
Environmental Science & Technology. 56:15207-15219
Many environmentally relevant poly-/perfluoroalkyl substances (PFASs) including perfluorooctane sulfonic acid (PFOS) and perfluorooctanoic acid (PFOA) exist in different isomeric (branched and linear) forms in the natural environment. The isomeric di
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6f5eb89fdab65458a3c6c685b66139a2
https://doi.org/10.1021/acs.est.2c05518
https://doi.org/10.1021/acs.est.2c05518
Autor:
Mitchell L. Passarelli, Samuel E. Wonfor, Andy X. Zheng, Yi C. Mazumdar, Jerry M. Seitzman, Adam M. Steinberg, Victor Salazar, Krishna Venkatesan, Michael Benjamin
Publikováno v:
AIAA SCITECH 2023 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2ffca539d52554dff535bb39410851a2
https://doi.org/10.2514/6.2023-0920
https://doi.org/10.2514/6.2023-0920
Autor:
Mitchell L. Passarelli, Askar Kazbekov, Victor Salazar, Krishna Venkatesan, Adam M. Steinberg
Publikováno v:
Proceedings of the Combustion Institute.
The effects of external forcing on a turbulent, liquid-fuelled, swirl-stabilized gas turbine combustor operating at a pressure of approximately 1 MPa are explored experimentally. In particular, the dynamics and coupling between the hydrodynamics, hea
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d610f1b437bc43f4dd97de97adbd428b
https://doi.org/10.1016/j.proci.2022.10.024
https://doi.org/10.1016/j.proci.2022.10.024
Publikováno v:
Proceedings of the Combustion Institute. 38:6105-6113
This paper demonstrates cross-frequency coupling between pressure, heat release rate, fuel spray and velocity oscillations in a model aeronautical gas turbine combustor operating at a pressure of approximately 10 atm. Heat release rate was characteri
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1b73a903c9d9cd0f7466c04be1ca9a95
https://doi.org/10.1016/j.proci.2020.06.177
https://doi.org/10.1016/j.proci.2020.06.177
Publikováno v:
Volume 3A: Combustion, Fuels, and Emissions.
Combustion dynamics is one of the most important factors to be understood and navigated in the design of modern gas turbine combustors. For liquid-fueled combustors this becomes especially challenging given the complexity of additional physics involv
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fc8e59a9b8e6ac85f3af26c5760374e6
https://doi.org/10.1115/gt2022-81745
https://doi.org/10.1115/gt2022-81745
Acoustic Flame Transfer Function Measurements in a Liquid Fueled High Pressure Aero-Engine Combustor
Publikováno v:
Volume 3A: Combustion, Fuels, and Emissions.
This paper describes an experimental approach and study of thermo-acoustic flame transfer functions in a high-pressure liquid-fueled rich burn combustor. The presence of high background flame luminosity in high-pressure sooty flame combustors preclud
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a2dd81d4c4be7436554efa2eb6262948
https://doi.org/10.1115/gt2022-81769
https://doi.org/10.1115/gt2022-81769
Autor:
Mitchell L. Passarelli, Samuel E. Wonfor, Andy X. Zheng, Sundar Ram Manikandan, Yi C. Mazumdar, Jerry M. Seitzman, Adam M. Steinberg, Hannah Bower, John Hong, Krishna Venkatesan, Michael Benjamin
Publikováno v:
AIAA SCITECH 2022 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fdde23231bc706ea1bd6aed361c139fb
https://doi.org/10.2514/6.2022-2347
https://doi.org/10.2514/6.2022-2347
Publikováno v:
AIAA Scitech 2020 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ff1b6d687ec8b5ca146c0532918f0b64
https://doi.org/10.2514/6.2020-0172
https://doi.org/10.2514/6.2020-0172
Publikováno v:
Combustion and Flame. 185:319-334
Dynamics of thermoacoustics oscillations occurring in a liquid fueled aeronautical gas turbine model combustor burning Jet A fuel were investigated experimentally at a pressure of approximately 10 bar. Data was acquired using 5 kHz repetition-rate st
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2c4435af5d2425225dddf4110a62b764
https://doi.org/10.1016/j.combustflame.2017.07.017
https://doi.org/10.1016/j.combustflame.2017.07.017
Publikováno v:
Proceedings of the Combustion Institute. 36:3873-3880
A framework is presented for analyzing the local instantaneous phase difference between non-stationary heat release rate and pressure oscillations that is appropriate for use in high-pressure liquid-fueled combustors. High-speed OH * chemiluminescenc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::84c3485b125d161e07629dda7b9f3fdb
https://doi.org/10.1016/j.proci.2016.08.032
https://doi.org/10.1016/j.proci.2016.08.032