Zobrazeno 1 - 10
of 32
pro vyhledávání: '"S. K. Sane"'
Publikováno v:
Journal of Propulsion and Power. 25:987-992
A Bayesian framework is developed for characterization of uncertainty in gas turbine performance predictions. Bayesian framework enables updating of uncertain parameters with availability of new information. Framework is demonstrated for a single spo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2a0cf62422d9acf0206a7b617cb80d01
https://doi.org/10.2514/1.38215
https://doi.org/10.2514/1.38215
Autor:
S. K. Sane, Shripad P. Mahulikar
Publikováno v:
Journal of Fluids Engineering. 127:1021-1028
This investigation analyzes the calibration nonlinearity of the ball-in-vortex flow-meter, designed to work on the principle of a rotating sphere in and due to a vortex flow. The comparison of this flow-meter reading with the standard flow-meter indi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b9945c65ac5049cee2fa8efb968d5f7c
https://doi.org/10.1115/1.1988342
https://doi.org/10.1115/1.1988342
Publikováno v:
Journal of Propulsion and Power. 18:907-912
In a mixed-stream turbofan, except for fan pressure ratio, the mission matched optimum selection of other basic cycle variables like bypass ratio, overall pressure ratio, throttle ratio, and turbine entry temperature depends upon engine-airframe inte
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::73f16ebfeca53646a3a2ccd6cf65011d
https://doi.org/10.2514/2.6016
https://doi.org/10.2514/2.6016
Publikováno v:
The Aeronautical Journal. 105:185-192
This paper begins with an outline of the procedure for predicting the infrared signature emissions from the airframe, engine casing, and the plume, and their attenuation by the intervening atmosphere. These emissions are contrasted against the backgr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e2726df5829f6c5309cb12920dc5213a
https://doi.org/10.1017/s0001924000025422
https://doi.org/10.1017/s0001924000025422
Publikováno v:
Journal of Aircraft. 35:380-386
Conceptual design has critical leverage on the entire course of design processes because it addresses the issue of selecting the baseline design to optimally accomplish the specified set of requirements. Conceptual-design software has been developed
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::784b0900644146103ea00a81231f74ec
https://doi.org/10.2514/2.2335
https://doi.org/10.2514/2.2335
Publikováno v:
IndraStra Global.
Simulation is a useful tool for design of a gas turbine engine, especially for control system design using hardware-in-loop simulation (HILS). The simulation must have real time engine performance prediction capabilities to be useful for HILS. The pa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f6f1ee840ac19ed6f975d6383012245c
http://dspace.library.iitb.ac.in/xmlui/handle/10054/7827
http://dspace.library.iitb.ac.in/xmlui/handle/10054/7827
Publikováno v:
38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
The paper presents a CFD based model for prediction of aerodynamic instabilities like rotating stall and surge in axial flow compressors. The model is based on quasi 3D Euler equations with source terms to represent momentum and energy transfer in th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d87e7a193415e77b3d80f29ce087504d
https://doi.org/10.2514/6.2002-4086
https://doi.org/10.2514/6.2002-4086
Autor:
S. K. Sane, Vivek Sanghi
Publikováno v:
International Journal of Turbo and Jet Engines. 16
The propulsion system has a high cost of ownership, long development period, and bears a dominant influence on aircraft mission performance. Thus identification of an optimum engine cycle right in the conceptual design, which makes the aircraft most
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::194da34ee77575fb1c88eb83c37e0a83
https://doi.org/10.1515/tjj.1999.16.1.27
https://doi.org/10.1515/tjj.1999.16.1.27
Publikováno v:
IndraStra Global.
Subsequent to identifying the optimum engine cycle over a specie ed baseline design mission, one of the important goals of conceptual design is to translate this into an aerothermomechanically compatible gas-e ow-path (GFP) layout and weight estimati
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8ddecbb7d57f6af877e6e99e4c297277
Autor:
S. K. Sane, R. W. Shende
Publikováno v:
Defence Science Journal. 38:439-456
Modern aircraft gas turbine engines depend heavily on squeeze film damper supports at the bearings for abatement of vibrations caused by a number of probable excitation sources. This design ultimately results in light-weight construction together wit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c2bd7dec21aa2cf01f80257fdf28829a
https://doi.org/10.14429/dsj.38.5874
https://doi.org/10.14429/dsj.38.5874