ArticleNature communications2025
Feasibility study of hydrogen-ammonia synergistic combustion in scramjets across broad Mach ranges.
Article in Nature communications, 2025. The graph could read no effect estimate from its abstract, so it casts no vote on the map. An erratum has been issued. Cited by 1 paper.
What it found
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The abstract states no effect estimate the extractor could read, or names no intervention and outcome on the map, so this paper lights no cell and moves no belief. It is still indexed, cited and linked below.
The trial behind it
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Who cites it
1 citing paper in PubMed.
- Comparative analysis of compressible solver schemes for underexpanded jet aerodynamics with Schlieren validation.Scientific reports · 2026Article
Corrections and comments
- Erratum issued
Authors and funding
7 authors.
Funding
Abstract
Ammonia shows advantages over hydrocarbon fuels for high-Mach scramjet engines, including superior cooling capacity and carbon-free combustion. However, its operation at lower Mach numbers remains challenging. Here, we successfully demonstrate ammonia-hydrogen ignition at Mach 3 and sustained combustion at Mach 6, confirming the feasibility of hydrogen-ammonia synergistic supersonic combustion. Compared to hydrogen combustion, ammonia addition at low Mach numbers does not alter flame paths but increases flame establishment times by 57.1% upstream and 100% downstream. Both global flame establishment and cavity ignition times are longer under the upstream scheme. At high Mach numbers, two distinct combustion modes are observed. Upstream hydrogen injection ignites more ammonia and produces more intense combustion than downstream injection. These results demonstrate the feasibility of ammonia-fueled scramjets operating across a broad Mach range.
Identifiers
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Registered trials
Read under generation 80e0d062 · epoch 390. Bibliography from PubMed, PubMed Central and OpenAlex; grants from NIH RePORTER; trial links from ClinicalTrials.gov; estimates, votes and beliefs from the OpenQuestion graph.