Zobrazeno 1 - 10
of 16
pro vyhledávání: '"Batchu, Suresh"'
Autor:
Venkatesh, Vishal, J., Sriraam, Vignesh D., Bala, K., Subhash, Velamati, Ratna Kishore, A.R., Srikrishnan, Ramakrishnananda, Balajee, Batchu, Suresh
Publikováno v:
In Aerospace Science and Technology June 2018 77:58-66
Publikováno v:
Proceedings of the National Aerospace Propulsion Conference ISBN: 9789811923777
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::81bc7156fbcc0f5af173859fdc73fdc0
https://doi.org/10.1007/978-981-19-2378-4_29
https://doi.org/10.1007/978-981-19-2378-4_29
Publikováno v:
Journal of Mines, Metals and Fuels. 69:117
The advanced gas turbine is designed to operate at higher temperature to increase thermal efficiency. Since the gas temperature exceed the allowable material temperature, so cooling techniques of turbine components are more important. Effusion film c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::64eda2ac237d24158c6ff6be8c9a0dfe
https://doi.org/10.18311/jmmf/2021/30139
https://doi.org/10.18311/jmmf/2021/30139
Publikováno v:
Proceedings of the National Aerospace Propulsion Conference ISBN: 9789811550386
The operating gas temperatures of advanced military aero engines are continuously increasing to achieve a higher specific thrust. The gas temperature exposed by hot end components is beyond material allowable temperature limits. It is essential to co
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9585cb24813e33ba91abf57de597aee1
https://doi.org/10.1007/978-981-15-5039-3_10
https://doi.org/10.1007/978-981-15-5039-3_10
Publikováno v:
Volume 1: Compressors, Fans, and Pumps; Turbines; Heat Transfer; Structures and Dynamics.
Improvement in specific thrust is one of the desirable requirements for Military aero-engine which has led to a tremendous increase in turbine inlet temperatures. This has resulted in combustion chambers to operate at a gas temperature of the order o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b0bf047146ef61147b7538b6efad73bb
https://doi.org/10.1115/gtindia2019-2480
https://doi.org/10.1115/gtindia2019-2480
Autor:
Batchu Suresh, Dhulesh Mirje
Publikováno v:
International Journal of Research in Engineering and Technology. :69-75
Increasing the creep life of gas turbine blades can be achieved by cooling the blades effectively. Film cooling is an effective method of cooling the blade surface. To improve the cooling effectiveness, recent attention has been given to contour the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0acc84dc65ccb26504975358b402267d
https://doi.org/10.15623/ijret.2016.0525012
https://doi.org/10.15623/ijret.2016.0525012
Publikováno v:
Crowns in Pediatric Dentistry
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9223101ee98d75081dfc505eae274c39
https://doi.org/10.5005/jp/books/12442_6
https://doi.org/10.5005/jp/books/12442_6