Output details
15 - General Engineering
University of Southampton
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Output 0 of 0 in the submission
Article title
Large-eddy simulation of kerosene spray combustion in a model scramjet chamber
Type
D - Journal article
Title of journal
Proceedings of the Institution of Mechanical Engineers Part G: Journal of Aerospace Engineering
Article number
-
Volume number
224
Issue number
9
First page of article
949
ISSN of journal
0954-4100
Year of publication
2010
Number of additional authors
3
Additional information
Significance of output:
Combustion efficiency of high-altitude rocket engine depends highly on flame stability. State-of-art numerical tools are used to investigate different combinations of pilot flame and fuel spray, which is difficult to measure from experiments.
Interdisciplinary
-
Cross-referral requested
-
Research group
None
Proposed double-weighted
No
Double-weighted statement
-
Reserve for a double-weighted output
No
Non-English
No
English abstract
-