Non-Uniform Nozzle Flow Heat Exchange Effects

Authors

  • J. N. Beri Scientific Analysis Group, New Delhi

DOI:

https://doi.org/10.14429/dsj.15.7260

Keywords:

Stagnation Temperature, Layer Effects, Heat Exchange

Abstract

Considering boundary layer effects in one-dimensional flow with heat exchange, true mean value flow parameters and their ratio to uniform free-stream values are derived. For one seventh power velocity distribution law and similar stagnation temperature and profiles variation in Mach number, stagnation temperature and impulse at the exit section are plotted versus boundary layer thickness.

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Published

2014-05-16

How to Cite

Beri, J. N. (2014). Non-Uniform Nozzle Flow Heat Exchange Effects. Defence Science Journal, 15(2), 85–92. https://doi.org/10.14429/dsj.15.7260

Issue

Vol. 15 No. 2

Section

Research Papers

License

 Where otherwise noted, the Articles on this site are licensed under Creative Commons License: CC Attribution-Noncommercial-No Derivative Works 2.5 India

 

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