Author Correction: Feasibility study of hydrogen-ammonia synergistic combustion in scramjets across broad Mach ranges
Year: 2026
Type: erratum
Abstract: In the version of the article initially published, there was a typographical error in the fourth paragraph of the Results section, where in the text now reading “Two inflow conditions are included in this study: 1) Inflow Mach number 1.60, stagnation temperature 640 K,” 640 appeared initially as “840,” while in next paragraph, in the text now reading “The equivalence ratio of ammonia (NH₃) is calculated based on the chemical reaction basis of generating NO 2 and H 2 O,” NO 2 appeared initially as “NO.” The errors are amended in the HTML and PDF versions of the article.
Source: Nature Communications
Institution: National University of Defense Technology
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: gold
Estimated APC paid: $6,990
OpenAlex ID: W7129070011