Using shock generator for the fuel mixing of the extruded single 4-lobe nozzle at supersonic combustion chamber.

Alizadeh A, Jasim DJ, Sohrabi N, Ahmed M, Ameer SA, Ibrahim SM, Dabis HK, Hussein AA, Sultan AJ

DOI: 10.1038/s41598-024-57103-0
Published: 2024 Mar 17
Container: Scientific reports
Publisher: Not recorded
Open access: yes

Credibility signals

limited evidence Score 45/100 under policy 1.0.0. This is a metadata assessment, not a judgment of the paper's conclusions.

Show all credibility signals

cautionDOI registered: No matching Crossref record was present in this response. Source: Crossref; license: CC0 metadata
cautionDOI resolves: No matching Crossref record was present in this response. Source: Crossref; license: CC0 metadata
not scoredDirectory of Open Access Journals: No matching DOAJ record was present in this response. No allow-list match; this is not evidence of low credibility. Source: DOAJ; license: CC0
not scoredMEDLINE indexed: Not checked or no result supplied; no credibility inference made. Source: No authority result supplied; license: Unknown
not scoredOpenAlex core source: Not checked or no result supplied; no credibility inference made. Source: No authority result supplied; license: Unknown
not scoredKnown publisher allow-list: Not checked or no result supplied; no credibility inference made. Source: No authority result supplied; license: Unknown
not scoredROR affiliation: Not checked or no result supplied; no credibility inference made. Source: No authority result supplied; license: Unknown
not scoredRetraction Watch retraction: No retraction notice matched this DOI in the deployed snapshot. No matching event found; coverage may be incomplete. Source: Retraction Watch; license: CC BY 4.0
not scoredRetraction Watch expression of concern: No expression of concern notice matched this DOI in the deployed snapshot. No matching event found; coverage may be incomplete. Source: Retraction Watch; license: CC BY 4.0
not scoredRetraction Watch correction: No correction notice matched this DOI in the deployed snapshot. No matching event found; coverage may be incomplete. Source: Retraction Watch; license: CC BY 4.0
not scoredRetraction Watch reinstatement: No reinstatement notice matched this DOI in the deployed snapshot. No matching event found; coverage may be incomplete. Source: Retraction Watch; license: CC BY 4.0
supportingOpen access status: Normalized open-access status: open. Source: Normalized work metadata; license: Caller-provided; provenance license not supplied to scorer
not scoredPublication license: Not checked or no result supplied; no credibility inference made. Source: No authority result supplied; license: Unknown
not scoredPublication version: A publication version was supplied but is not scored. Source: Normalized work metadata; license: Caller-provided; provenance license not supplied to scorer
cautionMetadata completeness: 5 of 6 scored descriptive metadata groups are present; missing fields increase uncertainty. Source: Normalized work metadata; license: Caller-provided; provenance license not supplied to scorer

Cite this work

BibTeX

@article{allodium:10.1038/s41598-024-57103-0,
  title = {Using shock generator for the fuel mixing of the extruded single 4-lobe nozzle at supersonic combustion chamber.},
  author = {Alizadeh A and Jasim DJ and Sohrabi N and Ahmed M and Ameer SA and Ibrahim SM and Dabis HK and Hussein AA and Sultan AJ},
  year = {2024},
  journal = {Scientific reports},
  doi = {10.1038/s41598-024-57103-0},
  url = {https://doi.org/10.1038/s41598-024-57103-0}
}

RIS

TY  - JOUR
TI  - Using shock generator for the fuel mixing of the extruded single 4-lobe nozzle at supersonic combustion chamber.
AU  - Alizadeh A
AU  - Jasim DJ
AU  - Sohrabi N
AU  - Ahmed M
AU  - Ameer SA
AU  - Ibrahim SM
AU  - Dabis HK
AU  - Hussein AA
AU  - Sultan AJ
PY  - 2024
JO  - Scientific reports
DO  - 10.1038/s41598-024-57103-0
UR  - https://doi.org/10.1038/s41598-024-57103-0
ER  -

APA

A, A., DJ, J., N, S., M, A., SA, A., SM, I., HK, D., AA, H., & AJ, S. (2024). Using shock generator for the fuel mixing of the extruded single 4-lobe nozzle at supersonic combustion chamber.. Scientific reports. https://doi.org/10.1038/s41598-024-57103-0

Source records

pubmed · retrieved 2026-09-26T09:42:40.694Z