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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:

Computational study of the multi hydrogen jets in presence of the upstream step in a Ma=4 supersonic flow
Xinglong Liu, Rasoul Moradi, Tran Dinh Manh, et al.
International Journal of Hydrogen Energy (2020) Vol. 45, Iss. 55, pp. 31118-31129
Closed Access | Times Cited: 28

Showing 1-25 of 28 citing articles:

Numerical investigation on mixing improvement mechanism of transverse injection based scramjet combustor
Gautam Choubey, Pabbala Monish Yadav, Yuvarajan Devarajan, et al.
Acta Astronautica (2021) Vol. 188, pp. 426-437
Closed Access | Times Cited: 80
Numerical investigation on a typical scramjet combustor using cavity floor H2 fuel injection strategy
Gautam Choubey, Malhar Solanki, Tathya Bhatt, et al.
Acta Astronautica (2022) Vol. 202, pp. 373-385
Open Access | Times Cited: 38
Influence of lateral single jets for thermal protection of reentry nose cone with multi-row disk spike at hypersonic flow: computational study
Yunbin Shi, Qiong Cheng, As’ad Alizadeh, et al.
Scientific Reports (2023) Vol. 13, Iss. 1
Open Access | Times Cited: 28
Numerical simulation of shock wave influence on flame diffusion characteristics in supersonic multi-strut combustor
Hongchao Qiu, Xingchi Wang, Hangyu Wu, et al.
Applied Thermal Engineering (2025), pp. 125542-125542
Closed Access | Times Cited: 1
Numerical investigation on geometric sensitivity and flame stabilisation mechanism in H2 fueled two-strut based scramjet combustor
Gautam Choubey, Parth Gaud, Abdulnasser Mahmood Fatah, et al.
Fuel (2021) Vol. 312, pp. 122847-122847
Closed Access | Times Cited: 51
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
Numerical study on the transverse jet flow and mixing characteristics of hydrogen/metal powder fuel in powder fuel scramjet
Hongming Ding, Changfei Zhuo, Xiong Chen, et al.
Fuel (2022) Vol. 326, pp. 125088-125088
Closed Access | Times Cited: 23
Research on combustion stability characteristics of scramjet combustor equipped with strut injector
Fuxu Quan, Juntao Chang, Chengkun Lv, et al.
Applied Thermal Engineering (2024) Vol. 258, pp. 124539-124539
Closed Access | Times Cited: 5
Investigation on the effect of the leading angle of the strut on the stabilisation characteristics of lifted jet flames
Zijian Zhao, Chaoyang Liu, Wei Huang
Acta Astronautica (2024) Vol. 224, pp. 520-532
Closed Access | Times Cited: 4
Mixing efficiency of hydrogen and air co-flow jets via wedge shock generator in dual-combustor ramjet
Yu Jiang, Nidal H. Abu‐Hamdeh, Rashad A. R. Bantan, et al.
Aerospace Science and Technology (2021) Vol. 116, pp. 106846-106846
Closed Access | Times Cited: 32
Numerical investigation on mixing enhancement of the cavity with pulsed jets under oblique shock wave interference
Jian Dai, Zuo Qiuru
Aerospace Science and Technology (2022) Vol. 123, pp. 107454-107454
Closed Access | Times Cited: 16
Three Dimensional CFD Analysis of two-strut assisted scramjet combustor
Gautam Choubey, Krutarth Dalal, Pratik Chavda, et al.
International journal of fluid mechanics research (2024) Vol. 51, Iss. 6, pp. 17-29
Closed Access | Times Cited: 2
Flow field reconstruction and shock train leading edge position detection of scramjet isolation section based on a small amount of CFD data
Hao Chen, Ye Tian, Mingming Guo, et al.
Advances in Aerodynamics (2022) Vol. 4, Iss. 1
Open Access | Times Cited: 9
Investigation of flow and combustion characteristics in a hydrogen-fueled scramjet combustor
Ming Yan, Ye Tian, Li Li, et al.
Journal of the Brazilian Society of Mechanical Sciences and Engineering (2024) Vol. 46, Iss. 9
Closed Access | Times Cited: 1
Effect of local equivalent ratio on spark ignition characteristics in a kerosene scramjet combustor at Mach 4 flight condition
Heng Bao, Daoning Yang, Lijun Yang, et al.
Aerospace Science and Technology (2024) Vol. 153, pp. 109460-109460
Closed Access | Times Cited: 1
Shock waves affected turbulent mixing region development in a strut-based scramjet combustor
X. Niu, Qian Chen
Acta Astronautica (2024) Vol. 225, pp. 107-119
Closed Access | Times Cited: 1
The heat flux research in hydrogen supersonic combustor at Mach number of 4
M. A. Goldfeld
International Journal of Hydrogen Energy (2021) Vol. 46, Iss. 24, pp. 13365-13376
Closed Access | Times Cited: 11
Evolution of the ignition and combustion process at high velocity at the channel entrance
M. A. Goldfeld
International Journal of Hydrogen Energy (2023) Vol. 48, Iss. 53, pp. 20483-20494
Closed Access | Times Cited: 4
Influence of cavity floor injection strategy on mixing improvement study of a splitter plate-assisted supersonic combustor
Gautam Choubey, Om Patel, Malhar Solanki, et al.
Engineering Analysis with Boundary Elements (2023) Vol. 155, pp. 995-1012
Closed Access | Times Cited: 4
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
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: 3
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
Influence of coolant multi-jets on heat reduction of nose cone with blunt spike at hypersonic flow
Mehdi Ghanbari, Soroush Maddah, Javad Alinejad
Scientific Reports (2022) Vol. 12, Iss. 1
Open Access | Times Cited: 3
Role of dual cavity on the combustion performance of a splitter plate-assisted supersonic combustor
Gautam Choubey, Sai Tanmay Veerendra Beeraka, Rishi Trivedi, et al.
International journal of fluid mechanics research (2024) Vol. 51, Iss. 6, pp. 1-15
Closed Access
LES investigation of a H2-fueled supersonic combustor: A two-strut injection approach
Gautam Choubey, Malhar Solanki, Sumit Tripathi, et al.
International Journal of Hydrogen Energy (2024) Vol. 91, pp. 1170-1183
Closed Access
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