Investigation of the mixing characteristics in a transverse hydrogen injection combustor with an inlet compression ramp
- Submitting institution
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Sheffield Hallam University
- Unit of assessment
- 12 - Engineering
- Output identifier
- 2870
- Type
- D - Journal article
- DOI
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10.1016/j.actaastro.2019.02.026
- Title of journal
- Acta Astronautica
- Article number
- -
- First page
- 479
- Volume
- 160
- Issue
- -
- ISSN
- 0094-5765
- Open access status
- Compliant
- Month of publication
- February
- Year of publication
- 2019
- URL
-
-
- Supplementary information
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- Request cross-referral to
- -
- Output has been delayed by COVID-19
- No
- COVID-19 affected output statement
- -
- Forensic science
- No
- Criminology
- No
- Interdisciplinary
- No
- Number of additional authors
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2
- Research group(s)
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-
- Proposed double-weighted
- No
- Reserve for an output with double weighting
- No
- Additional information
- In collabration with University of Science and Technology of China and funded by the National Natural Science Foundation of China (Grant No. 91441117 and 51576182) this work aimed to improve the mixing process by introducing an inlet compression ramp, while mixing mechanism can be enhanced by shock wave train interacting with fuel and air.
- Author contribution statement
- -
- Non-English
- No
- English abstract
- -