Computing supersonic non-premixed turbulent combustion by an SMLD flamelet progress variable model
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- 作者：A. Coclitea ; b ; alessandro.coclite@poliba.it" class="auth_mail" title="E-mail the corresponding author ; L. Cutronec ; b ; l.cutrone@cira.it" class="auth_mail" title="E-mail the corresponding author ; M. Gurtnerd ; gurtner@lfa.mw.tum.de" class="auth_mail" title="E-mail the corresponding author ; P. De Palmaa ; b ; pietro.depalma@poliba.it" class="auth_mail" title="E-mail the corresponding author ; O.J. Haidnd ; haidn@lfa.mw.tum.de" class="auth_mail" title="E-mail the corresponding author ; G. Pascazioa ; b ; giuseppe.pascazio@poliba.it" class="auth_mail" title="E-mail the corresponding author
- 关键词：Joint presumed PDF modelling ; Hydrogen&ndash ; air combustion ; Reynolds-averaged Navier&ndash ; Stokes equations
- 刊名：International Journal of Hydrogen Energy
- 出版年：2016
- 出版时间：5 January 2016
- 年：2016
- 卷：41
- 期：1
- 页码：632-646
- 全文大小：3500 K
文摘
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An improved model for non-premixed supersonic turbulent combustion is proposed.
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Statistically most likely distribution is used in a flamelet/progress-variable model.
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The complex structure of the supersonic H2–air flame is correctly predicted.