Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Tushar Sikroria"'
Publikováno v:
Fluids, Vol 8, Iss 2, p 73 (2023)
The quest for the physical mechanisms underlying turbulent high-speed jet flows is underpinned by the extraction of spatio-temporal coherent structures from their flow fields. Experimental measurements to enable data decomposition need to comprise ti
Externí odkaz:
https://doaj.org/article/30f080db24134d42ae90fa34b6264623
Publikováno v:
AIAA Journal. 60:3749-3759
Publikováno v:
14th International Symposium on Particle Image Velocimetry. 1
Motivated by applications in the propulsion industry, the fundamental study of phase-locked shear-layer instabilities in supersonic impinging jets has been of research interest for long time. While such flows have been experimentally investigated in
Publikováno v:
International Journal of Petrochemical Science & Engineering. 4:109-115
In Fluidized Bed Catalytic Cracking (FCC) process, hydrocarbon feed undergoes vapour phase cracking in presence of hot regenerated catalyst to produce valuable products like LPG, Gasoline and Diesel. FCC feed injection system is most critical hardwar
Autor:
Abhijit Kushari, Tushar Sikroria
Publikováno v:
Journal of Engineering for Gas Turbines and Power. 143
This paper presents the experimental analysis of the impact of swirl number of cross-flowing air stream on liquid jet spray trajectory at a fixed air flow velocity of 42 m/s with the corresponding Mach number of 0.12. The experiments were conducted f
Publikováno v:
AIAA AVIATION 2020 FORUM.
The flow unsteadiness in supersonic impinging jets due to the aero-acoustic feedback loop phenomenon can lead to practical problems like ground erosion in short take-off and vertical landing (STOVL) aircrafts, high noise levels and high unsteady stru
Autor:
Tushar Sikroria, Abhijit Kushari
Publikováno v:
Journal of Engineering for Gas Turbines and Power. 141
This paper presents detailed analysis of an experimental investigation of the impact of swirl number of subsonic cross-flowing air stream on liquid jet breakup at an airflow Mach number of 0.12, which is typical in gas turbine conditions. Experiments
Publikováno v:
Journal of Engineering for Gas Turbines and Power. 136
This paper presents the results of an experimental investigation of liquid jet breakup in a cross-flow of air under the influence of swirl (swirl numbers 0 and 0.2) at a fixed air flow Mach No. 0.12 (typical gas turbine conditions). The experiments h
Publikováno v:
ASME 2013 Gas Turbine India Conference.
This paper presents the results of an experimental investigation of liquid jet breakup in a cross-flow of air under the influence of swirl (swirl numbers 0 and 0.2) at a fixed air flow Mach No. 0.12 (typical gas turbine conditions). The experiments h
Publikováno v:
Fluids; Feb2023, Vol. 8 Issue 2, p73, 17p