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OpenAlex Citation Counts

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OpenAlex is a bibliographic catalogue of scientific papers, authors and institutions accessible in open access mode, named after the Library of Alexandria. It's citation coverage is excellent and I hope you will find utility in this listing of citing articles!

If you click the article title, you'll navigate to the article, as listed in CrossRef. If you click the Open Access links, you'll navigate to the "best Open Access location". Clicking the citation count will open this listing for that article. Lastly at the bottom of the page, you'll find basic pagination options.

Requested Article:

Hydrogen mixing augmentation mechanism induced by the vortex generator and oblique shock wave in a scramjet engine
Zhao-bo Du, Chibing Shen, Wei Huang, et al.
International Journal of Hydrogen Energy (2022) Vol. 47, Iss. 46, pp. 20232-20253
Closed Access | Times Cited: 9

Showing 9 citing articles:

Improving the combustion of scramjet engines with struts using grooves and bumps
Zhi-qiang Sheng, Lan Zhang, Liang-ze Lu, et al.
Aerospace Science and Technology (2024) Vol. 147, pp. 109047-109047
Closed Access | Times Cited: 6
Enhancing the mixing characteristics of multi-hydrogen jets in scramjet engines through the implementation of fuel injection strategies and vortex generator positioning
Kaiqiang Liu, Yu Pan, Mysoon M. Al‐Ansari, et al.
Fuel (2023) Vol. 355, pp. 129466-129466
Open Access | Times Cited: 15
Numerical investigation of mixing enhancement in a cavity-based supersonic combustor using the upstream wavy wall
Kaifeng Wang, Cao Wei
International Journal of Hydrogen Energy (2025) Vol. 114, pp. 18-30
Closed Access
Effects of flight dynamic pressure on plume temperature distribution and heat release characteristic in the kerosene-fueled scramjet
Weiguang Cai, Shu Zheng, Qingxuan Jia, et al.
Physics of Fluids (2025) Vol. 37, Iss. 4
Closed Access
Effects of lifted fuel injection using an upstream ramp of a cavity on scramjet combustion
Yu Dan, Zhi-qiang Sheng, Lan Zhang, et al.
Aerospace Science and Technology (2023) Vol. 142, pp. 108651-108651
Closed Access | Times Cited: 11
Effect of strut profile, angled injection, and blunting of leading edge on mixing of supersonic hydrogen-air streams
Ankit Singh, Sudipto Mukhopadhyay
International Journal of Hydrogen Energy (2022) Vol. 48, Iss. 3, pp. 1175-1188
Closed Access | Times Cited: 14
Positional effect of vortex generators on the combustion efficiency of the micro combustor fuelled with hydrogen/air mixture
P. Booma Devi, Mysoon M. Al‐Ansari, Nora Dahmash Al- Dahmash, et al.
Fuel (2023) Vol. 358, pp. 130309-130309
Closed Access | Times Cited: 4
Numerical study on the mixing enhancement induced by the interaction between the hydrogen/air coaxial jets and oblique shock wave at Mach 3 supersonic crossflow
Hao-ran Tang, Chibing Shen, Zhao-bo Du, et al.
International Journal of Hydrogen Energy (2023) Vol. 48, Iss. 92, pp. 36122-36141
Closed Access | Times Cited: 2
Influence of Incident Shocks on Flame Characteristics in the Strut-Equipped Supersonic Combustor
Junlong Zhang, Libo Lin, Y. Kai, et al.
AIAA Journal (2022) Vol. 61, Iss. 1, pp. 76-85
Closed Access | Times Cited: 3
Research on the mixing characteristics of a cavity based supersonic combustion chamber coupled with secondary recirculation jets
Jian Dai, Long Chen, Fanchao Kong
International Journal of Hydrogen Energy (2024) Vol. 92, pp. 516-526
Closed Access
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