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Abstract
Various snags in the fuel system of a military turbojet engine are analyzed and the effect on the engine performance is studied. Causes of the defects and remedial measures suggested to address such snags are also highlighted in this paper.
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References
- Cohen, H., Rogers, G.F.C. and Saravanamuttoo, H.I.H., "Gas turbine Theory", Longman Group Limited, 1996.
- Mishra, R.K., Mishra, A.K. and Gouda, G., "Causes and Remedies of High Jet Pipe Temperature in Turbo Shaft Engines: Case Studies", Journal of Aerospace Sciences and Technologies, Vol. 62, No.3, August, 2010, pp. 203-208.
- Philip P Walsh and Paul Fletcher., "Gas Turbine Performance", 2004, Blackwell Science Ltd.
- Jayasimha, K.S., Mishra, R.K. and Mistry, S.N., "Defect Trend Analysis for a Turbojet Engine: Case Studies", Journal of Aerospace Sciences and Technologies, Vol.63, No.4, November, 2011, pp.334-338.
References
Cohen, H., Rogers, G.F.C. and Saravanamuttoo, H.I.H., "Gas turbine Theory", Longman Group Limited, 1996.
Mishra, R.K., Mishra, A.K. and Gouda, G., "Causes and Remedies of High Jet Pipe Temperature in Turbo Shaft Engines: Case Studies", Journal of Aerospace Sciences and Technologies, Vol. 62, No.3, August, 2010, pp. 203-208.
Philip P Walsh and Paul Fletcher., "Gas Turbine Performance", 2004, Blackwell Science Ltd.
Jayasimha, K.S., Mishra, R.K. and Mistry, S.N., "Defect Trend Analysis for a Turbojet Engine: Case Studies", Journal of Aerospace Sciences and Technologies, Vol.63, No.4, November, 2011, pp.334-338.