Effect of Fuel-Injection Distance and Cavity Rear-Wall Height on the Flameholding Characteristics in...
Effect of Fuel-Injection Distance and Cavity Rear-Wall Height on the Flameholding Characteristics in a Mach 2.52 Supersonic Flow
About this item
Full title
Author / Creator
He, Zhonghao , Wang, Hongbo , Li, Fan , Tian, Yifu , Wan, Minggang and Zhu, Jiajian
Publisher
Basel: MDPI AG
Journal title
Language
English
Formats
Publication information
Publisher
Basel: MDPI AG
Subjects
More information
Scope and Contents
Contents
The ethylene-fueled flameholding characteristics of a cavity-based scramjet combustor are experimentally and numerically investigated. The test facility used the air heater, which heats air from room temperature to total temperature 1477 K. A nozzle is installed behind the heater outlet to increase the air speed to Mach 2.52. Two cavity geometries...
Alternative Titles
Full title
Effect of Fuel-Injection Distance and Cavity Rear-Wall Height on the Flameholding Characteristics in a Mach 2.52 Supersonic Flow
Authors, Artists and Contributors
Author / Creator
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Primary Identifiers
Record Identifier
TN_cdi_doaj_primary_oai_doaj_org_article_cbad3ab9fbed4c8286fcb77ee9036e7d
Permalink
https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_doaj_primary_oai_doaj_org_article_cbad3ab9fbed4c8286fcb77ee9036e7d
Other Identifiers
ISSN
2226-4310
E-ISSN
2226-4310
DOI
10.3390/aerospace9100566
