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Efficient utilization of heat sink of hydrocarbon fuel for regeneratively cooled scramjet

Author
WEN BAO1 ; XIANLING LI1 ; JIANG QIN1 ; WEIXING ZHOU1 ; DAREN YU1
[1] School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China
Source

Applied thermal engineering. 2012, Vol 33-34, pp 208-218, 11 p ; ref : 20 ref

ISSN
1359-4311
Scientific domain
Energy
Publisher
Elsevier, Kidlington
Publication country
United Kingdom
Document type
Article
Language
English
Author keyword
Chemical reaction Heat sink Heat transfer Hydrocarbon fuel Scramjet
Keyword (fr)
Condition opératoire Craquage Dissipateur thermique Fissuration Flux chaleur Flux thermique Modèle 1 dimension Modélisation Refroidissement Système refroidissement Température maximale Transfert chaleur Vitesse écoulement Statoréacteur à combustion supersonique
Keyword (en)
Operating conditions Cracking(refining) Heat sink Cracking Heat flux Heat flow One dimensional model Modeling Cooling Cooling system Maximum temperature Heat transfer Flow velocity Scramjet
Keyword (es)
Condición operatoria Craqueo Disipador térmico Agrietamiento Flujo térmico Modelo 1 dimensión Modelización Enfriamiento Sistema enfriamiento Temperatura máxima Transferencia térmica Velocidad flujo
Classification
Pascal
001 Exact sciences and technology / 001D Applied sciences / 001D06 Energy / 001D06D Energy. Thermal use of fuels / 001D06D02 Theoretical studies. Data and constants. Metering / 001D06D02B Heat transfer

Discipline
Energy
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
24736019

Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS

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