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Effect of cooling channel geometry on re-cooled cycle performance for hydrogen fueled scramjet

Author
BAO, W1 ; QIN, J1 ; ZHOU, W. X1 ; YU, D. R1
[1] School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China
Source

International journal of hydrogen energy. 2010, Vol 35, Num 13, pp 7002-7011, 10 p ; ref : 32 ref

CODEN
IJHEDX
ISSN
0360-3199
Scientific domain
General chemistry, physical chemistry; Energy
Publisher
Elsevier, Kidlington
Publication country
United Kingdom
Document type
Article
Language
English
Author keyword
Channel geometry Fuel Re-Cooled Cycle Regenerative cooling Scramjet
Keyword (fr)
Analyse paramétrique Analyse sensibilité Aéronef Capacité calorifique Géométrie Hydrodynamique Hydrogène Optimisation Performance Véhicule Statoréacteur à combustion supersonique
Keyword (en)
Parametric analysis Sensitivity analysis Aircraft Heat capacity Geometry Hydrodynamics Hydrogen Optimization Performance Vehicle Scramjet
Keyword (es)
Análisis sensibilidad Aeronave Capacidad calorífica Geometría Hidrodinámica Hidrógeno Optimización Rendimiento Vehículo
Classification
Pascal
001 Exact sciences and technology / 001D Applied sciences / 001D06 Energy / 001D06B Fuels / 001D06B06 Alternative fuels. Production and utilization / 001D06B06B Hydrogen

Discipline
Energy
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
23065707

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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