Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Umesh Bhayaraju"'
Publikováno v:
Volume 4A: Combustion, Fuels and Emissions.
A generic novel injector was designed for multi-Lean Direct Injection (M-LDI) combustors. One of the drawbacks of the conventional pressure swirl and prefilming type airblast atomizers is the difficulty of obtaining a uniform symmetric spray under al
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::38e08cb0de4acdad44d4dbf3c3d0f320
https://doi.org/10.1115/gt2017-63981
https://doi.org/10.1115/gt2017-63981
Publikováno v:
Volume 4A: Combustion, Fuels and Emissions.
The Combustion and Fire Research Laboratory (CFRL) at the University of Cincinnati (UC) is working on the development of advanced next generation injectors for DLN combustors. Several inputs were received from the project partners during the developm
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::843e92bd006fbc87c52e7d5298b6ed02
https://doi.org/10.1115/gt2017-63976
https://doi.org/10.1115/gt2017-63976
Publikováno v:
Volume 4A: Combustion, Fuels and Emissions.
In the present investigation, a novel fuel injection concept is developed for Dry Low NOx combustors. A multi-injector block is used for fuel-air mixing and flame stabilization. The injectors in the multi-injector block are equally spaced in a rectan
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2a602cf5edcff4c2826245a7fb90c377
https://doi.org/10.1115/gt2016-56722
https://doi.org/10.1115/gt2016-56722
Publikováno v:
Volume 4A: Combustion, Fuels and Emissions.
A novel airblast injector is designed for gas turbine combustors. Unlike standard pressure swirl and prefilming/non-prefilming air blast atomizers, the novel injector is designed to improve the fuel injection delivery to the injector and improve atom
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cdf0894094691c9bb89a64841c931536
https://doi.org/10.1115/gt2016-56340
https://doi.org/10.1115/gt2016-56340
Autor:
Christoph Hassa, Umesh Bhayaraju
Publikováno v:
Atomization and Sprays. 19:1147-1169
Liquid sheet breakup of a prefilming and nonprefilming airblast atomizer is investigated experimentally at ambient temperatures and elevated pressures of air. The breakup is studied by High-Speed flow visualization. The visualizations show the differ
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c8a2ad7f4df99de44b02f768f67c9c69
https://doi.org/10.1615/atomizspr.v19.i12.50
https://doi.org/10.1615/atomizspr.v19.i12.50
Publikováno v:
Journal of Engineering for Gas Turbines and Power. 138
In the present study, two measurement techniques are adopted to evaluate the fuel–air mixing under atmospheric conditions using an industrial fuel–air premixer. These techniques are CO2 mixing and planar laser induced fluorescence (PLIF) in water
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8b8931b56bb401fc67417757c6a91647
https://doi.org/10.1115/1.4031528
https://doi.org/10.1115/1.4031528
Publikováno v:
Volume 4A: Combustion, Fuels and Emissions.
In the present study, two measurement techniques are adopted to evaluate the fuel-air mixing under atmospheric conditions using an industrial fuel-air pre-mixer. These techniques are CO2 mixing and Planar Laser Induced Fluorescence (PLIF) in water. I
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::aa82f740b3aa9a60c7fda027bc5fc0cf
https://doi.org/10.1115/gt2015-42747
https://doi.org/10.1115/gt2015-42747
Publikováno v:
Volume 2: Combustion, Fuels and Emissions, Parts A and B.
Gas turbine combustors with lean combustion injectors are prone to thermo-acoustic/combustion instabilities. Several passive techniques have been developed to control combustion instabilities, such as using Helmholtz resonators or viscous dampers usi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::103760dfbe49d5e0057373f085f1bf4a
https://doi.org/10.1115/gt2010-22616
https://doi.org/10.1115/gt2010-22616
Publikováno v:
16th AIAA/CEAS Aeroacoustics Conference.
To control combustion instabilities occurring in LPP gas turbine combustors, several active and passive systems have been developed in recent years. The combustion chamber cooling geometry has the potential to influence instability feedback loops by
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::42c991f3edf6d2ae8e1594a8d6408c44
https://doi.org/10.2514/6.2010-3929
https://doi.org/10.2514/6.2010-3929