Zobrazeno 1 - 5
of 5
pro vyhledávání: '"T. N. Satish"'
Autor:
A Vivek, T. N. Satish, G. Uma, Mangalanathan Umapathy, U. Chandrasekhar, G Kiran, A. N. V. Rao, SN Anagha
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 234:342-360
Blade tip clearance is a critical engine health parameter measured on gas turbines. Increase in tip clearance results in decreased efficiency, whereas with decrease in clearance due to thermal and centrifugal loads, rotor blades might rub the engine
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::58b76d10c34f08336976393ec18ab634
https://doi.org/10.1177/0954410019865853
https://doi.org/10.1177/0954410019865853
Autor:
Mangalanathan Umapathy, Anagha S. Nambiar, G. Uma, A. N. Vishwanatha Rao, T. N. Satish, V. P. S. Naidu, Soumemndu Jana
Publikováno v:
Proceedings of the National Aerospace Propulsion Conference ISBN: 9789811550386
Developmental testing of gas turbine propulsion systems involves iterative experimental studies right from First Engine to Test (FETT) till production release. During initial design validation tests, engines require dedicated instrumentation for carr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8e199b109e9bfc39afb3a27d788e99bc
https://doi.org/10.1007/978-981-15-5039-3_16
https://doi.org/10.1007/978-981-15-5039-3_16
Publikováno v:
Proceedings of the National Aerospace Propulsion Conference ISBN: 9789811550386
Rotor blade vibration in turbomachinery has been a major cause of failure due to HCF, often resulting in catastrophic damage. The primary aeromechanical design concerns are blade flutter and forced vibration that need to be quantified. The severity o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0bf995a88998618dc833f5ef41a9ea5b
https://doi.org/10.1007/978-981-15-5039-3_15
https://doi.org/10.1007/978-981-15-5039-3_15
Autor:
A.S. Nambiar, G. Uma, U. Chandrashekhar, A. N. V. Rao, T. N. Satish, Vijay Petley, Mangalanathan Umapathy
Publikováno v:
Experimental Techniques. 42:575-592
The rotor tip clearance is a vital parameter to characterize turbomachinery performance. It is an essential measurement during engine development and testing. The efficiency of the major modules like fan, compressor and turbine depends on the optimum
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a4b83e26dcd491ebd6cfcd8351669e91
https://doi.org/10.1007/s40799-018-0281-y
https://doi.org/10.1007/s40799-018-0281-y
Autor:
Vijay Petley, U. Chandrasekhar, Mangalanathan Umapathy, T. N. Satish, G. Uma, K. P. Rakesh, A. N. V. Rao
Publikováno v:
Experimental Techniques. 41:131-138
This study presents a concerted approach developed for experimental measurement of surface temperature of critical aeroengine components using a non non-intrusive sensor that is compatible with structural integrity and endurance requirements of high
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2c2bc710ac2980499b6799150c6fcf98
https://doi.org/10.1007/s40799-016-0162-1
https://doi.org/10.1007/s40799-016-0162-1