Please use this identifier to cite or link to this item: http://nopr.niscpr.res.in/handle/123456789/29734
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dc.contributor.authorBharani, Sanjeev-
dc.contributor.authorSingh, S N-
dc.contributor.authorAgrawal, D P-
dc.date.accessioned2014-11-05T10:48:14Z-
dc.date.available2014-11-05T10:48:14Z-
dc.date.issued1997-10-
dc.identifier.issn0975-1017 (Online); 0971-4588 (Print)-
dc.identifier.urihttp://hdl.handle.net/123456789/29734-
dc.description167-177en_US
dc.description.abstractAn attempt has been made to analyze flow in the outer annulus of an annular reverse-flow combustor using a realistic using 1200 sector model with realistic design. Velocity distribution has been measured in the outer annulus for two inlet conditions and the flow split through dilution, primary and cooling holes have been evaluated. It is observed that the flow split through the turn-section rows of cooling holes as well as swirlers and the inner annulus does not get affected significantly by the change in the inlet conditionsen_US
dc.language.isoen_USen_US
dc.publisherNISCAIR-CSIR, Indiaen_US
dc.rights CC Attribution-Noncommercial-No Derivative Works 2.5 Indiaen_US
dc.sourceIJEMS Vol.04(5) [October 1997]en_US
dc.titleSector model: An approach for experimental studies of gas turbine combustorsen_US
dc.typeArticleen_US
Appears in Collections:IJEMS Vol.04(5) [October 1997]

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