Non-Uniform Nozzle Flow Heat Exchange Effects

  • 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.
Published
2014-05-16
How to Cite
Beri, J. (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
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