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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:

Influence of coaxial fuel–air jets on mixing performance of extruded nozzle at supersonic combustion chamber: Numerical study
Xiaoling Shi, Dunlan Song, Hui Tian, et al.
Physics of Fluids (2023) Vol. 35, Iss. 5
Closed Access | Times Cited: 32

Showing 1-25 of 32 citing articles:

Comparison of the different shapes of extruded annular nozzle on the fuel mixing of the hydrogen jet at supersonic combustion chamber
Yaohui Li, Zhu Guang-hui, Yanpu Chao, et al.
Energy (2023) Vol. 281, pp. 128142-128142
Closed Access | Times Cited: 24
Using shock generator for the fuel mixing of the extruded single 4-lobe nozzle at supersonic combustion chamber
As’ad Alizadeh, Dheyaa J. Jasim, Neaman Sohrabi, et al.
Scientific Reports (2024) Vol. 14, Iss. 1
Open Access | Times Cited: 11
Flow field reconstruction from spray imaging: A hybrid physics-based and machine learning approach based on two-phase fluorescence particle image velocimetry measurements
Fengnian Zhao, Ziming Zhou, David L. S. Hung, et al.
Physics of Fluids (2024) Vol. 36, Iss. 4
Closed Access | Times Cited: 5
Usage of double injector for efficient mixing of the fuel behind the ramp injector at supersonic combustion chamber
Ihab Omar, Mohamed R. El-Sharkawy, Rifaqat Ali, et al.
Scientific Reports (2025) Vol. 15, Iss. 1
Open Access
Investigation of the injector configurations of ramp injection system for efficient hydrogen mixing inside the combustor of scramjet engine
Yassine Bouazzi, Ali B.M. Ali, Loghman Mostafa, et al.
International Journal of Hydrogen Energy (2025)
Closed Access
Prediction of the transient coolant jet released from the nose cone at supersonic flow via machine learning
Asad Ali, M. Yasiri, Pooya Ghodratallah, et al.
Scientific Reports (2025) Vol. 15, Iss. 1
Open Access
Thermally guided streamline placement for joint flow and scalar field visualization
Xueyang Shen, Yanci Zhang
The Visual Computer (2025)
Closed Access
Effect of thermal boundary condition and turbulent models on the combustion simulation of ethylene-fueled scramjet combustor
Yujia Sun, Shu Zheng, Lin Jiang, et al.
Physics of Fluids (2023) Vol. 35, Iss. 9
Closed Access | Times Cited: 10
Improvement of fuel mixing of single ejected 2-lobe fuel injector using shock generator at supersonic flow
Hossein Seraj, Farhad Hosseinnejad, Yasser Rostamiyan, et al.
International Journal of Hydrogen Energy (2023) Vol. 50, pp. 939-950
Closed Access | Times Cited: 10
Usage of multi-extruded nozzles for hydrogen fuel mixing in the double cavity flame holder in the existence of the shock generator
Naser Kamyarpour, Farhad Hosseinnejad, Seyyed Masoud Seyyedi, et al.
International Journal of Hydrogen Energy (2024) Vol. 64, pp. 301-308
Closed Access | Times Cited: 3
Usage of extruded diamond multi-injectors for improvement of fuel mixing inside the supersonic combustion chamber
Hossein Seraj, Farhad Hosseinnejad, Yasser Rostamiyan, et al.
Scientific Reports (2023) Vol. 13, Iss. 1
Open Access | Times Cited: 9
Influence of the non-equal aligned nozzles for fuel injection inside the supersonic combustion chamber
Zhongmian Fan, Lingxiao Wang, Fei Xu, et al.
Scientific Reports (2024) Vol. 14, Iss. 1
Open Access | Times Cited: 3
Fuel mixing and diffusion behind the unswept ramp injector with lobed nozzle at combustor of scramjet engine
Seyyed Amirreza Abdollahi, Seyyed Faramarz Ranjbar, Mir Biuok Ehghaghi
Energy (2024) Vol. 308, pp. 133089-133089
Closed Access | Times Cited: 3
Insights into flame flashback phenomenon utilizing a Strut-Cavity flame holder inside scramjet combustor
Singeetham Pranaykumar, Anup Ghosh
Physics of Fluids (2024) Vol. 36, Iss. 11
Closed Access | Times Cited: 3
Enhancing fuel distribution of downward steps in supersonic combustion chambers using shock generators
Naser Kamyarpour, Farhad Hosseinnejad, Seyyed Masoud Seyyedi, et al.
International Journal of Modern Physics C (2024) Vol. 35, Iss. 11
Closed Access | Times Cited: 2
The usage of non-aligned multi-circular winding injectors for efficient fuel mixing inside the scramjet engine
Naim Ben Ali, Ali Basem, Pooya Ghodratallah, et al.
Energy (2024) Vol. 298, pp. 131403-131403
Closed Access | Times Cited: 2
Computational modeling of the rectangular non-aligned multi-injector for efficient fuel mixing in a supersonic combustion chamber
Pan Zhang, Zhen Li, Seyyed Amirreza Abdollahi
Scientific Reports (2024) Vol. 14, Iss. 1
Open Access | Times Cited: 2
Estimation of the fuel mixing of annular extruded fuel multi-jets in cavity flame holder at the supersonic combustion chamber via predictive surrogate model
Dechen Wei, Yuanyuan Jiao, Yukun Fan
Engineering Analysis with Boundary Elements (2024) Vol. 163, pp. 369-377
Closed Access | Times Cited: 1
The role of annular 2-lobe nozzle in a strut injection system on the mechanism of fuel distribution at a scramjet engine
Dechen Wei, Yuanyuan Jiao, Ning Zhang, et al.
Energy (2024) Vol. 301, pp. 131679-131679
Closed Access | Times Cited: 1
Computational study of transverse oblique injectors for improvement of fuel mixing in scramjet engine of supersonic vehicles
Haicui Wang, Zhimin Ma, Jing Bian, et al.
Energy (2024) Vol. 306, pp. 132389-132389
Closed Access | Times Cited: 1
Effect of shock generator on fuel mixing in an annular single lobe transverse nozzle at the supersonic combustion chamber of a scramjet engine using computational fluid dynamics
Dechen Wei, Yuanyuan Jiao, Ning Zhang, et al.
Energy (2023) Vol. 283, pp. 128515-128515
Closed Access | Times Cited: 3
Application of multi-extruded fuel injectors for mixing enhancement of hydrogen gas at scramjet engine: computational study
Seyyed Amirreza Abdollahi, Seyyed Faramarz Ranjbar, Saman Aminian, et al.
Scientific Reports (2023) Vol. 13, Iss. 1
Open Access | Times Cited: 3
Fuel mixing enhancement of transverse coaxial air and fuel jet by upstream shock wave on in scramjet engines: numerical study
Seyyed Amirreza Abdollahi, Moharram Jafari, Saman Aminian, et al.
Scientific Reports (2023) Vol. 13, Iss. 1
Open Access | Times Cited: 2
Using extruded circular multi-injectors to improve fuel jet mixing and distribution in combustion chambers of scramjet
Dian Huang
Energy (2023) Vol. 288, pp. 129696-129696
Closed Access | Times Cited: 2
The role of the shock generator on the mixing performance of hydrogen jet released from the extruded transverse 3-lobe nozzle in a scramjet engine
Zuocai Dai, Yunhe Zou, Limeng Chow
Energy (2023) Vol. 288, pp. 129831-129831
Closed Access | Times Cited: 2
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