CFD analysis to investigate the effect of rotor tip clearance on the performance of a 2:1 pressure ratio fan stage
IR@NAL: CSIR-National Aerospace Laboratories, Bangalore
View Archive Info| Field | Value | |
| Title |
CFD analysis to investigate the effect of rotor tip clearance on the performance of a 2:1 pressure ratio fan stage
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| Creator |
Shobhavathy, MT
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| Subject |
Propellants and Fuels
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| Description |
This paper describes the numerical studies carried out to investigate the effect of rotor tip clearance on the performance of a 2:1 pressure ratio fan stage. The first part of the work includes evaluation of the commercial CFD tool ANSYS FLUENT with the fan stage at design speed having no rotor tip clearance. The flow structure of the baseline configuration was studied with the help of Mach number contour and velocity vector plots.
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| Date |
2013
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| Type |
Conference or Workshop Item
PeerReviewed |
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| Format |
application/msword
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| Identifier |
http://nal-ir.nal.res.in/11877/1/16002.doc
Shobhavathy, MT (2013) CFD analysis to investigate the effect of rotor tip clearance on the performance of a 2:1 pressure ratio fan stage. In: National Propulsion Conference 2013, 21 Feb 2013, Indian Institute of Madras, Chennai. |
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| Relation |
http://nal-ir.nal.res.in/11877/
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