Zobrazeno 1 - 10
of 18
pro vyhledávání: '"Shailendra Naik"'
Autor:
Hrishikesh K. Chavan, Shubham T. Chavan, Saumya Koul, Shubham Kumar, Shailendra Naik, Rajib Kumar Sinharay
Publikováno v:
Proceeding of International Conference on Computational Science and Applications ISBN: 9789811908620
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7cd9dd6c0aff24f3f8b40798311fad54
https://doi.org/10.1007/978-981-19-0863-7_22
https://doi.org/10.1007/978-981-19-0863-7_22
Publikováno v:
European Conference on Turbomachinery Fluid Dynamics and Thermodynamics.
Sequentially stacked impingement channels allow for a more effective use of the cooling fluid and can limit the heat transfer reduction due to the crossflow when the number of jets increases. In this paper, sequential impingement channels are experim
Autor:
Johannes Eitenmüller, Christoph Lyko, Tom Ostrowksi, Heinz-Peter Schiffer, Sebastian Leichtfuss, Shailendra Naik, Manuel Wilhelm, Leonhard Gresser
Publikováno v:
Volume 2B: Turbomachinery.
High pressure turbines are nowadays designed to a point where most design enhancements only yield marginal efficiency improvements. This challenges research facilities to reliably resolve ever smaller differences in efficiency caused by individual de
Autor:
Shailendra Naik
Publikováno v:
Heat Exchangers-Design, Experiment and Simulation
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1e273673e9af5d678fcb6a36f61a1339
https://doi.org/10.5772/67323
https://doi.org/10.5772/67323
Publikováno v:
World Journal of Clinical Infectious Diseases. 7:21
Antioxidant enzyme profile of two clinical isolates of Entamoeba histolytica varying in sensitivity to antiamoebic drugs
Publikováno v:
Volume 5A: Heat Transfer.
The trailing edge region of gas turbine blades is generally subjected to extremely high external heat loads due to the combined effects of high mach numbers and gas temperatures. In order to maintain the metal temperatures of these trailing edges to
Publikováno v:
Volume 5A: Heat Transfer.
The leading edge regions of first stages blades and vanes of heavy-duty gas turbines are subjected to high thermal loads. Efficient cooling allows the reduction of the coolant mass flow required to drive the metal temperatures to a range satisfying m
Publikováno v:
Heat and Mass Transfer. 38:7-16
The film cooling performance on a convex surface subjected to zero and favourable pressure gradient free-stream flow was investigated. Adiabatic film cooling effectiveness values were obtained for five different injection geometries, three with cylin