Zobrazeno 1 - 10
of 24
pro vyhledávání: '"R K Satpathy"'
Publikováno v:
Defence Science Journal. 72:135-145
Legacy turbojet engines suffer degradation in performance with usage. Degradations in engine components show different observable symptoms based on the control mode of the engine. Hence, to accurately model the engine and its degradations, a novel of
Publikováno v:
Applications of Microscopy in Materials and Life Sciences ISBN: 9789811629815
Orientation stability of a unique rotated-Brass (rBs)-{110}\(\left\langle {556} \right\rangle\) texture during cold rolling of an Al–Zn–Mg–Cu-based 7010 aluminium alloy has been systematically investigated by X-ray diffraction, electron back-sc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2e3e2e95226f9ea5cdee95ee4821447c
https://doi.org/10.1007/978-981-16-2982-2_16
https://doi.org/10.1007/978-981-16-2982-2_16
Publikováno v:
Journal of Failure Analysis and Prevention. 17:529-538
Military aircraft engines operate under arduous environmental conditions with rapid throttle excursions as a part of its mission requirements. Life of an aircraft engine particularly of a military class is limited by the longevity of hot end componen
Publikováno v:
Advances in Structural Integrity ISBN: 9789811071966
Turbine blades of a military gas turbine are one of the most safety-critical components as per MIL-STD-1783 as its failure cannot be contained by engine casing in case of failure. Statistic tells, the major failure of the turbine blade is due to fati
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f69493cd7f9b702c4638b22c9d4eeb51
https://doi.org/10.1007/978-981-10-7197-3_53
https://doi.org/10.1007/978-981-10-7197-3_53
Autor:
C S Shastry and R K Satpathy
Publikováno v:
Proceedings of Indian National Science Academy, Vol 47, Iss 4A (2015)
Complex Angular Momentum Approach to Nuclear Scattering: A Review
Publikováno v:
International Journal of Turbo & Jet-Engines. 32
A highly loaded full-scale annular combustor is studied in the air-flow facility for the effect of operating variables such as compressor discharge velocity and fuel-air ratio on the performance parameters. The combustor is designed to operate at hig
Isothermal Fatigue Behaviour of Two Nickelbase Alloys for Turbine Blades of Fighter Aircraft Engines
Publikováno v:
ASME 2013 Gas Turbine India Conference.
Turbine blades of fighter class aero-engines are subjected to repeated and unsteady throttle excursions during exploitation leading to thermo-mechanical fatigue. Failures of few turbine blades have led to premature withdrawals and major accidents. He
Publikováno v:
Polymer International. 38:227-232
Twenty polystyrene-g-gelatin samples were synthesised using Ce(IV) as the free radical initiator in order to make biodegradable polystyrene. Recovery of polystyrene from acid hydrolysis of the grafted sample and the appearance of new bands of gelatin
Autor:
B K Das, R K Satpathy
Publikováno v:
Journal of Physics G: Nuclear and Particle Physics. 18:1431-1435
The authors respond to comments by Puri and Gupta (see ibid., vol.16, p.221 (1990)) on their previous work.