Design, Development and Experimental Evaluation of Reverse Flow Combustor
IR@NAL: CSIR-National Aerospace Laboratories, Bangalore
View Archive Info| Field | Value | |
| Title |
Design, Development and Experimental Evaluation of Reverse Flow Combustor
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| Creator |
Muralidhara, HS
Muthu Selvan, G Vinod Kumar, Vyas Jeyaseelan, AR Rajeshwari Natarajan, S Hariharan, R Satish Kumar, M |
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| Subject |
Aircraft Propulsion and Power
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| Description |
A Typical reverse flow combustor is developed for an application in a small gas turbine engine. This is designed for 4 kg/s air flow rate, 6 bar pressure and 1000K exit temperature. This is designed from first principles and fine tuned with Computational Fluid Dynamics (CFD) technique. Combustor is developed and experimentally evaluated in a test rig of Combustion Laboratory of National Aerospace Laboratories (NAL). Inlet to the test rig is compressed dry air at ambient temperature. Combustor performance parameters such as combustion efficiency, total pressure loss and exit temperature pattern factor is presented. Effects of equivalence ratios on these combustion performance parameters are discussed.
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| Date |
2013-12-13
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| Type |
Conference or Workshop Item
PeerReviewed |
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| Format |
application/pdf
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| Identifier |
http://nal-ir.nal.res.in/12183/1/cp241.pdf
Muralidhara, HS and Muthu Selvan, G and Vinod Kumar, Vyas and Jeyaseelan, AR and Rajeshwari Natarajan, S and Hariharan, R and Satish Kumar, M (2013) Design, Development and Experimental Evaluation of Reverse Flow Combustor. In: National Conference on IC engines and combustion, 13 Dec 2013, NIT,surat. |
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| Relation |
http://nal-ir.nal.res.in/12183/
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