Author Correction: Feasibility study of hydrogen-ammonia synergistic combustion in scramjets across broad Mach ranges

Nature Communications 2026 Open access

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Authors: Xin Song, Zun Cai, Jianheng Ji, Zihang Chen, Taiyu Wang, Fan Li, Mingbo Sun
DOI: 10.1038/s41467-026-69757-7
Cited by: 1

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.

Fields of Study & Subjects

Combustion and flame dynamics Rocket and propulsion systems research Computational Fluid Dynamics and Aerodynamics

Publication details

Journal / source
Nature Communications
Publisher
Springer Science and Business Media LLC
Volume
17
Issue
1
Pages
1659–1659
Publication date
16 February 2026
Language
EN