Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Sandeep Kedukodi"'
Autor:
David Gomez-Ramirez, Sandeep Kedukodi, Yong Kim, Ram Srinivasan, Srinath V. Ekkad, Hee-Koo Moon
Publikováno v:
Applied Thermal Engineering. 114:65-76
Modern combustor design optimization is contingent on the accurate characterization of the combustor flame side heat loads. The present work focuses on the experimental measurement of the isothermal (non-reacting) convective heat transfer along a fus
Autor:
Srinath V. Ekkad, Yong Kim, Siddhartha Gadiraju, Ram Srinivasan, Suhyeon Park, David Gomez-Ramirez, Sandeep Kedukodi, Hee-Koo Moon
Publikováno v:
Journal of Engineering for Gas Turbines and Power. 140
Designing gas turbine combustors requires accurate measurement and prediction of the violent, high-temperature environment in reacting flow. One important factor in combustor design is the heat load on the inner surface of the combustor liner during
Autor:
Sandeep Kedukodi, Srinath V. Ekkad, Suhyeon Park, Siddhartha Gadiraju, Ram Srinivasan, Yong Kim
Publikováno v:
Volume 5C: Heat Transfer.
Numerical methods coupled with experimental benchmarking approaches, are typically used as effective tools for solving engineering problems due to their significant time saving benefits. In this paper, the swirling flow through an industrial lean-pre
Autor:
Srinath V. Ekkad, David Gomez-Ramirez, Ram Srinivasan, Hee-Koo Moon, Sandeep Kedukodi, Yong Kim
Publikováno v:
Volume 2: Heat Transfer in Multiphase Systems; Gas Turbine Heat Transfer; Manufacturing and Materials Processing; Heat Transfer in Electronic Equipment; Heat and Mass Transfer in Biotechnology; Heat Transfer Under Extreme Conditions; Computational Heat Transfer; Heat Transfer Visualization Gallery; General Papers on Heat Transfer; Multiphase Flow and Heat Transfer; Transport Phenomena in Manufacturing and Materials Processing.
The current computational study deals with the isothermal fluid flow and heat transfer analysis of a gas turbine combustor subject to different boundary conditions. A 90 degree sector model was studied computationally in order to identify the impinge
Autor:
Sandeep Kedukodi, Srinath V. Ekkad
Publikováno v:
ASME 2015 Gas Turbine India Conference.
Established numerical approaches for performing detailed flow analysis happens to be an effective tool for industry based applied research. In the present study, computations are performed on multiple gas turbine combustor geometries for turbulent, n
Publikováno v:
Volume 5C: Heat Transfer.
Numerical computations are performed on three configurations of a model gas turbine combustor geometry for cold flow conditions. The purpose of this study is to understand the effect of changes to combustor passage section on the location of peak con