Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Giridhara Babu Yepuri"'
Autor:
Giridhara Babu Yepuri, Karthick Raja Kaliraj, Kishor Kumar, Felix Jesuraj, Jayakumar Janardanan Sarasamma
Publikováno v:
Volume 1: Compressors, Fans, and Pumps; Turbines; Heat Transfer; Structures and Dynamics.
Various studies have been carried out related to the labyrinth seals and reported in the open literature using the different seal arrangements at the stator-rotor seal cavity region. In the present study, numerical analysis has been carried out for t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::79151b72780f05374932b0cb7abf8ccf
https://doi.org/10.1115/gtindia2019-2397
https://doi.org/10.1115/gtindia2019-2397
Publikováno v:
Journal of The Institution of Engineers (India): Series C. 99:393-400
Increasing the gas turbine inlet temperature is one of the key technologies in raising gas turbine engine power output. Film cooling is one of the efficient cooling techniques to cool the hot section components of a gas turbine engines in turn the tu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::739d443bbad3ca4a130dccd5c4923798
https://doi.org/10.1007/s40032-016-0302-5
https://doi.org/10.1007/s40032-016-0302-5
Autor:
Balaji Sankar, Brijeshkumar J Shah, Giridhara Babu Yepuri, Jeyaseelan Ar, Sundaram, Mohana, Poornima N, Natarajan, Rajeshwari, Sadanand S Kulkarni, Santhosh Kumar Sahadevan, R Shambhoo, Shri, Srinivas J, Tahzeeb Hassan Danish, THENNAVARAJAN SUBRAMANIAN, Manjunath Pulumathi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2b5ad604f8e73b342664cc4425be90b2
Publikováno v:
Procedia Engineering. 127:398-404
Film cooling is one of the cooling techniques used in gas turbines to protect the blades from high temperature. The efficiency of gas turbine can be increased by increasing the inlet gas temperature. The present study aims at numerical investigation
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f9ae1532906af99fc7043a06570956d9
Publikováno v:
ASME 2015 Gas Turbine India Conference.
The experimental investigation of adiabatic film cooling effectiveness is carried out on a flat plates with 4:1 scaled up hole geometries, similar to that of typical turbine nozzle guide vane film cooling holes. Under this study, three flat plate mod
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6977f14a8901656f725f7db56cd2b016
https://doi.org/10.1115/gtindia2015-1394
https://doi.org/10.1115/gtindia2015-1394
Autor:
Kumar Gottekre Narayanappa, Vivek Sasikumar, Raghavan Rajendran, Giridhara Babu Yepuri, Felix Jesuraj, Sinith Poozhiyil
Publikováno v:
ASME 2015 Gas Turbine India Conference.
The gas turbine combustor liner which is subjected to high temperature requires efficient cooling. In earlier days concept of slot film cooling is utilized in the combustion liners and in modern combustors multiple row film cooling (effusion cooling)
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8da05f265735a52f4918b5f3992a95a4
https://doi.org/10.1115/gtindia2015-1377
https://doi.org/10.1115/gtindia2015-1377