Numerical simulation on thermal decomposition of n-dodecane using CFD with reaction model

Numerical simulation on thermal decomposition of n-dodecane using CFD with reaction model

A thermal protection makes one of the biggest technical concerns for a reusable hypersonic flight vehicle. A regenerative cooling using fuel should be promising candidate to clear this problem. In general, a liquid hydrocarbon fuel has worse cooling capability than cryogenic fuel like liquid hydroge...

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Bibliographic Details
Main Authors: Tatsushi ISONO, Takuto MIYAURA, Yu DAIMON, Takuo ONODERA, Sadatake TOMIOKA
Format: Article
Language:English
Published: The Japan Society of Mechanical Engineers 2024-09-01
Series:Journal of Fluid Science and Technology
Subjects:
fuel heating experiment
computational fluid dynamics (cfd)
reaction modeling
thermal decomposition
supercritical state
regenerative cooling
liquid hydrocarbon fuel
hypersonic flight vehicle
Online Access:https://www.jstage.jst.go.jp/article/jfst/19/4/19_2024jfst0032/_pdf/-char/en
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