Corpus ID: 110339718

Compressed Gas parameters at Different Pressures in Convergent Divergent Nozzle of an Aircraft Engine

@inproceedings{Satyanand2014CompressedGP,
  title={Compressed Gas parameters at Different Pressures in Convergent Divergent Nozzle of an Aircraft Engine},
  author={G. Satyanand and Prateek Kishore and B. Sadhana},
  year={2014}
}
The fighter aircraft, consists of two engines and the engine sections are inlet, compressor, combustor, turbine, exhaust, the gas energy is accelerated through the convergent- divergent duct shape, to obtain more useful jet thrust, the velocity of the gas which is coming out of the nozzle and the formation of the shock inside the nozzle depends on back pressure of the nozzle so, in this thesis the compressed gas parameters of a convergent-divergent nozzle at different pressures inside the… Expand

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