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 backward-facing step on the mixing efficiency of multi microjets at supersonic flow
Zhixiong Li, Rasoul Moradi, Seyed Maziar Marashi, et al.
Acta Astronautica (2020) Vol. 175, pp. 37-44
Closed Access | Times Cited: 50

Showing 1-25 of 50 citing articles:

Influence of trapezoidal lobe strut on fuel mixing and combustion in supersonic combustion chamber
Yu Jiang, Masoud Hajivand, Hosein Sadeghi, et al.
Aerospace Science and Technology (2021) Vol. 116, pp. 106841-106841
Closed Access | Times Cited: 103

Recent research progress on transverse injection technique for scramjet applications-a brief review
Gautam Choubey, Yuvarajan Devarajan, Wei Huang, et al.
International Journal of Hydrogen Energy (2020) Vol. 45, Iss. 51, pp. 27806-27827
Closed Access | Times Cited: 121

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

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

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 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

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

Effect of injection scheme on asymmetric phenomenon in rectangular and circular scramjets
Guangwei Ma, Mingbo Sun, Guoyan Zhao, et al.
Chinese Journal of Aeronautics (2022) Vol. 36, Iss. 1, pp. 216-230
Open Access | Times Cited: 22

Influence of flow control schemes of the three-strut injector on the mixing efficiency and total pressure loss for a scramjet combustor
Yongqiang Chen, Guangming Guo, Juliang Han, et al.
International Journal of Hydrogen Energy (2023) Vol. 48, Iss. 94, pp. 36972-36986
Closed Access | Times Cited: 13

Combustion performance in a cavity-based combustor under subatmospheric pressure
Zhixin Zhu, Yakun Huang, Huangwei Zhang, et al.
Fuel (2021) Vol. 302, pp. 121115-121115
Closed Access | Times Cited: 29

Numerical investigation of cavity-induced enhanced supersonic mixing with inclined injection strategies
Jian Dai, Zuo Qiuru, Chao Huang
Acta Astronautica (2021) Vol. 180, pp. 630-638
Closed Access | Times Cited: 28

Effects of sawtooth grooves on supersonic combustion
Lan Zhang, Zhi-qiang Sheng, Yu Dan
Aerospace Science and Technology (2023) Vol. 136, pp. 108223-108223
Closed Access | Times Cited: 11

Assessment on the supersonic combustor performance induced by the asymmetric struts with hydrogen fuel
Chunlei Li, Yingkun Li, Xiong Chen, et al.
International Journal of Hydrogen Energy (2020) Vol. 45, Iss. 53, pp. 29560-29578
Closed Access | Times Cited: 24

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: 15

Effect of jet schemes of the double-nozzle strut injector on mixing efficiency of air and hydrogen for a scramjet combustor
Yongqiang Chen, Guangming Guo, Juliang Han, et al.
International Journal of Hydrogen Energy (2022) Vol. 47, Iss. 53, pp. 22633-22649
Closed Access | Times Cited: 15

Inlet static pressure ratio effect on vortex structure downstream of the flameholder in subsonic–supersonic mixing flow
Yakun Huang, Zhaohui Yao, Zhixin Zhu, et al.
Physics of Fluids (2023) Vol. 35, Iss. 9
Closed Access | Times Cited: 8

Research on a novel combined shock control mechanism for thermal protection and drag reduction in hypersonic compressible flow field
Zekang Wang, Xiaobing Zhang
International Journal of Heat and Mass Transfer (2022) Vol. 201, pp. 123592-123592
Closed Access | Times Cited: 12

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

Numerical study on the induced-ramp mixed and combustion characteristics of rocket-based combined cycle engine
Jian Dai, Chao Huang, Fei Xu, et al.
Aerospace Science and Technology (2021) Vol. 118, pp. 107068-107068
Closed Access | Times Cited: 15

Study on backward-facing step flow and heat transfer characteristics of hybrid nanofluids
Cong Qi, Zi Ding, Jianglin Tu, et al.
Journal of Thermal Analysis and Calorimetry (2020)
Closed Access | Times Cited: 13

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: 8

A Survey of Flow Field and Combustion Characteristics under Subatmospheric Pressure
Guoyu Ding, Zhaohui Yao, Zhixiang Zhu, et al.
Aerospace (2024) Vol. 11, Iss. 5, pp. 387-387
Open Access | Times Cited: 1

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