Transition mechanisms in cross-flow-dominated hypersonic flows with free-stream acoustic noise
- Submitting institution
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University of Wolverhampton
- Unit of assessment
- 12 - Engineering
- Output identifier
- 1608
- Type
- D - Journal article
- DOI
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10.1017/jfm.2020.346
- Title of journal
- Journal of Fluid Mechanics
- Article number
- ARTN A21
- First page
- -
- Volume
- 896
- Issue
- -
- ISSN
- 0022-1120
- Open access status
- Compliant
- Month of publication
- June
- Year of publication
- 2020
- 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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1
- Research group(s)
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-
- Proposed double-weighted
- No
- Reserve for an output with double weighting
- No
- Additional information
- The findings of this work enhanced the understanding of the complex physical mechanism of transition, which can provide explanation for the ambiguities observed in previous experimental data and support the development of new computational models for accurate description of the transition process. The results of this work were disseminated in international conferences and meetings and contributed to the research activity of the team NATO Applied Vehicle Technology AVT-240 on "hypersonic boundary-layer transition prediction". The work subsequently gained recognition through a NATO Panel Excellence award from AVT-240.
- Author contribution statement
- -
- Non-English
- No
- English abstract
- -