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pro vyhledávání: '"G. V. Ramana Murty"'
Publikováno v:
Universal Journal of Mechanical Engineering. 2:163-168
This paper examines the effect of twist in diffuser vane from hub to shroud on the performance of an industrial centrifugal compressor stage. The chosen diffuser has an aerofoil section with varying blade chord from hub to shroud due to blade twist o
Publikováno v:
Fluid Mechanics and Fluid Power – Contemporary Research ISBN: 9788132227410
The effect of variation of diffuser radius ratio on the performance of a centrifugal compressor stage with vaneless diffuser (VLD), low solidity vaned diffuser (LSVD), and twisted vaned diffuser (TVD) was studied using Computational Fluid Dynamics (C
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::48597c8b5bdf9e00e0cfea6d2e384ba4
https://doi.org/10.1007/978-81-322-2743-4_86
https://doi.org/10.1007/978-81-322-2743-4_86
Publikováno v:
Journal of Mechanical Engineering and Sciences, Vol 1, Pp 75-86 (2011)
Aerodynamic studies in the static components of a centrifugal compressor stage were conducted using the computational fluid dynamics solver FLUENT. For the simulation study, a typical centrifugal compressor stage geometry with a flow coefficient of 0
Publikováno v:
International Journal of Fluid Machinery and Systems. 3:11-19
The performance of the crossover system of a centrifugal compressor stage consisting of static components of U-bend, return channel vanes and exit ducting with a bend is investigated. This study is confined to the assessment of performance of the cro
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy. 218:637-646
The present investigation is undertaken to study the performance of an existing stage of an industrial centrifugal compressor with a vaneless diffuser and is aimed at improving the efficiency of the compressor stage through the use of a low-solidity
Publikováno v:
Volume 6: Turbo Expo 2005, Parts A and B.
Numerical simulation of impeller and low solidity vaned diffuser (LSD) of a centrifugal compressor stage is performed individually using CFX- BladeGen and BladeGenPlus codes. The tip mach number for the chosen study was 0.35. The same configuration w
Autor:
Prasad Mukkavilli, G. Rama Raju, Abhijit Dasgupta, G. V. Ramana Murty, K. V. Jagadeshwar Chary
Publikováno v:
Volume 5: Turbo Expo 2002, Parts A and B.
Diffusers are found to play a significant role in the performance of centrifugal compressors. Extensive studies have been in progress in various research laboratories for improvement of performance with various types of diffusers. One such effort for
Autor:
G. V. Ramana Murty, N. Venkatrayulu
Publikováno v:
Volume 1: Turbomachinery.
The effect of incidence on the generation and growth of secondary flows in a linear turbine cascade was studied in the present investigations using a Variable Density Cascade Tunnel at an exit Mach number of 0.43 and a Reynolds number of 8 × 105. Th
Publikováno v:
Scopus-Elsevier
The results of experimental studies on a centrifugal compressor stage using uncambered constant thickness low solidity diffuser vanes (LSD) are reported in this paper. In the present work, efforts are concentrated for study of stage performance with
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d1b7f0229d45bfb5841dc176c3c121e3
http://www.scopus.com/inward/record.url?eid=2-s2.0-21544479119&partnerID=MN8TOARS
http://www.scopus.com/inward/record.url?eid=2-s2.0-21544479119&partnerID=MN8TOARS
Autor:
G. V. Ramana Murty
Publikováno v:
Artha Vijnana: Journal of The Gokhale Institute of Politics and Economics. 16:365
In recent years, the World Bank Atlas has become a widely used source of information on population and per capita income in all countries of the world. The latest Atlas converts the G.N.P. figures of the individual countries expressed in local curren