Publication2023
Computational assessment of performance parameters of an aero gas turbine combustor for full flight envelope operation
The record
- Type
- Publication
- Date
- 1 December 2023
- Level
- National
- Journal
- International Journal of Turbo and Jet Engines
- Volume
- 40
- Issue
- 4
- Pages
- 481-491
- Published
- 1 December 2023
- DOI
- 10.1515/tjj-2021-0034
- Scopus ID
- 85115603127
- ISSN
- 03340082
- Authors
- 3
- Open access
- No
- Citations
- 0
- International co-authorship
- No
- Co-author countries
- IN
Classification
Every label below carries the reasoning it was assigned on, the confidence band it was assigned in, and what produced it. The rubric is published.
UN Sustainable Development Goals
9.5 Enhance scientific research, upgrade technological capabilities, and increase researchers and R&D spending
CFD analysis of aero gas turbine combustor performance parameters across flight envelope conditions advances high-performance aerospace engine design
- High confidence
- The subject matter is a strong and direct inference from the record type, the funding or organising body, or the programme context, even where the title alone is thin. Example: an ICMR-funded project against SDG 3, on the strength of the agency.
- Judged
- Judged against the published classification rubric, under the rubric and prompt versions recorded with the run that produced it.
- Produced by
- claude-haiku-4-5-20251001, under kortex-publication-v1
Viksit Bharat @2047
vb-3.1 Research and development
Aerospace engineering research contributes to research and development capabilities
- Produced by
- claude-haiku-4-5-20251001, under kortex-publication-v1
Each label above carries the instrument and the version that produced it. How each classification is reached.
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- Source rows resolved into this record
- 1
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Citing this record
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KIIT Deemed to be University. “Computational assessment of performance parameters of an aero gas turbine combustor for full flight envelope operation”. Kortex.