Overview and analysis of the experimentally measured throat heat transfer in liquid rocket engine thrust chambers
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference63 articles.
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4. Effect of uncooled inlet length and nozzle convergence angle on the turbulent boundary layer and heat transfer in conical nozzles operating with air;Boldman;J. Heat Transfer,1967
5. A simple equation for rapid estimation of rocket nozzle convective heat transfer coefficients;Bartz;J. Jet Propuls.,1957
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