Zobrazeno 1 - 10
of 11
pro vyhledávání: '"Mahesh K. Varpe"'
Publikováno v:
ASME 2021 Gas Turbine India Conference.
In a transonic compressor rotor, tip leakage flow interacts with passage shock, casing boundary layer and secondary flow. This leads to increase in total pressure loss and reduction of compressor stability margin. Casing treatment is one of the passi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f0b01728a11971bf817f0460b60f9d5e
https://doi.org/10.1115/gtindia2021-75882
https://doi.org/10.1115/gtindia2021-75882
Publikováno v:
ASME 2021 Gas Turbine India Conference.
In the present research work, effect of airfoil vortex generator on performance and stability of transonic compressor stage is investigated through CFD simulations. In turbomachines vortex generators are used to energize boundary and generated vortex
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ce66a87d1706a08fcf1adf6a739bc1d7
https://doi.org/10.1115/gtindia2021-75881
https://doi.org/10.1115/gtindia2021-75881
Autor:
Mahesh K. Varpe, P. Sreekumar
Publikováno v:
Volume 1: Compressors, Fans, and Pumps; Turbines; Heat Transfer; Structures and Dynamics.
The aerodynamics design of a steam turbine stage is an agreement between the performance requirements and the mechanical limitations. The design of last stage of the low-pressure steam (LP) turbine is the most complicated because of the blade twist a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ba9e06d138a5c2961368ab965c9452be
https://doi.org/10.1115/gtindia2019-2509
https://doi.org/10.1115/gtindia2019-2509
Autor:
Mahesh K. Varpe, R. Deeksha
Publikováno v:
Volume 2: Combustion, Fuels, and Emissions; Renewable Energy: Solar and Wind; Inlets and Exhausts; Emerging Technologies: Hybrid Electric Propulsion and Alternate Power Generation; GT Operation and Maintenance; Materials and Manufacturing (Including Coatings, Composites, CMCs, Additive Manufacturing); Analytics and Digital Solutions for Gas Turbines/Rotating Machinery.
Wind energy has become one of the vital sustainable energy resources and a leading contender to the renewable resources race. The need of extending the aerodynamic performance of a wind turbine paved the way for radical approaches in the design of wi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::88b68c4a7c349444443f380adbc0b9ce
https://doi.org/10.1115/gtindia2019-2541
https://doi.org/10.1115/gtindia2019-2541
Autor:
D. S. Swasthika, Mahesh K. Varpe
Publikováno v:
Volume 2: Combustion, Fuels, and Emissions; Renewable Energy: Solar and Wind; Inlets and Exhausts; Emerging Technologies: Hybrid Electric Propulsion and Alternate Power Generation; GT Operation and Maintenance; Materials and Manufacturing (Including Coatings, Composites, CMCs, Additive Manufacturing); Analytics and Digital Solutions for Gas Turbines/Rotating Machinery.
In wind turbine blade, most of the losses occurs due to aerodynamic losses in the post stall operating condition. Adoption of the blade leading edge tubercles improves the post stall aerodynamic performance. Nevertheless the geometric parameters of t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::af1e600aa83bc31b54c46d74135d9a28
https://doi.org/10.1115/gtindia2019-2548
https://doi.org/10.1115/gtindia2019-2548
Publikováno v:
Volume 1: Compressors, Fans and Pumps; Turbines; Heat Transfer; Combustion, Fuels and Emissions.
Winglets are plane surfaces with certain thickness and different shapes. Winglets are used in aircraft to reduce wing tip vortex which is created due to differential pressure in between pressure surface and suction surface. In transonic axial compres
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::31d8511c02742dbd6f5a2ff3c042c46f
https://doi.org/10.1115/gtindia2017-4686
https://doi.org/10.1115/gtindia2017-4686
Autor:
Mahesh K. Varpe, A. M. Pradeep
Publikováno v:
International Journal of Gas Turbine, Propulsion and Power Systems. 6:17-26
This paper explores the effect of a prescribed intense shear flow on the flow structures in an axial flow compressor cascade. An approximate shear flow is generated in the test section of an open circuit cascade wind tunnel by using a planar grid of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::306296e8ca6a5400045f9afcfc45123f
https://doi.org/10.38036/jgpp.6.2_17
https://doi.org/10.38036/jgpp.6.2_17
Autor:
Mahesh K. Varpe, A. M. Pradeep
Publikováno v:
IndraStra Global.
This paper describes the design of a nonaxisymmetric hub contouring in a shroudless axial flow compressor cascade operating at near stall condition. Although an optimum tip clearance (TC) reduces the total pressure loss, further reduction in the loss
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::790c06120ad3ad68caf50deba021913f
https://igi.indrastra.com/items/show/56996
https://igi.indrastra.com/items/show/56996
Autor:
Mahesh K. Varpe, A. M. Pradeep
Publikováno v:
Volume 2A: Turbomachinery.
This paper describes the design of a non-axisymmetric hub contouring in a shroudless axial flow compressor cascade operating at near stall condition. Although, an optimum tip clearance reduces the total pressure loss, further minimization of the loss
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::810ef2209ad1f2617926ac95d37831a2
https://doi.org/10.1115/gt2014-26725
https://doi.org/10.1115/gt2014-26725
Autor:
A. M. Pradeep, Mahesh K. Varpe
Publikováno v:
International Journal of Rotating Machinery, Vol 2013 (2013)
This paper explores the effect of inlet shear flow on the tip leakage flow in an axial flow compressor cascade. A flow with a high shear rate is generated in the test section of an open circuit cascade wind tunnel by using a combination of screens wi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::57fbd65604d04c38bcd66c10c098422d