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Heat Transfer Research
Fator do impacto: 0.404 FI de cinco anos: 0.8 SJR: 0.264 SNIP: 0.504 CiteScore™: 0.88

ISSN Imprimir: 1064-2285
ISSN On-line: 2162-6561

Volumes:
Volume 50, 2019 Volume 49, 2018 Volume 48, 2017 Volume 47, 2016 Volume 46, 2015 Volume 45, 2014 Volume 44, 2013 Volume 43, 2012 Volume 42, 2011 Volume 41, 2010 Volume 40, 2009 Volume 39, 2008 Volume 38, 2007 Volume 37, 2006 Volume 36, 2005 Volume 35, 2004 Volume 34, 2003 Volume 33, 2002 Volume 32, 2001 Volume 31, 2000 Volume 30, 1999 Volume 29, 1998 Volume 28, 1997

Heat Transfer Research

DOI: 10.1615/HeatTransRes.v38.i1.20
pages 9-20

Modeling the Process of Afterburning in Supersonic Jets

K. B. Galitseiskii
Moscow Aviation Institute (State Technical University), Russian Federation

RESUMO

Heat transfer in a high-velocity underexpanded turbulent two-phase jet was studied on the basis of numerical modeling and the distributions of basic gasdynamic and thermal parameters, viz., velocity, temperature and concentration of the gas mixture components in the jet were determined. The process of afterburning of a high-velocity jet in atmosphere was investigated. The impact of the concentration of Al2O3 particles in the jet on its thermal gasdynamic parameters is analyzed.


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