OpenAlex Citation Counts

OpenAlex Citations Logo

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:

An experimental investigation of the effects of upstream probe disturbance on compressor cascade performance
Honghui Xiang, Ning Ge, Minjie Hou, et al.
Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering (2016) Vol. 231, Iss. 7, pp. 1248-1257
Closed Access | Times Cited: 12

Showing 12 citing articles:

Effects of the airfoil probes on the aerodynamic performance of a transonic compressor cascade
Qingdian Zhang, Hongwei Ma, Yafei Zhong, et al.
Aerospace Science and Technology (2023) Vol. 136, pp. 108227-108227
Closed Access | Times Cited: 6

Manipulating near-wall flow instability and transport characteristics by the airfoil probe: Investigation on a transonic compressor cascade
Qingdian Zhang, Hongwei Ma, Zhongqiang Xie, et al.
Physics of Fluids (2023) Vol. 35, Iss. 8
Closed Access | Times Cited: 5

Experimental Study of the Vibration Phenomenon of Compressor Rotor Blade Induced by Inlet Probe Support
Yong Yang, Honghui Xiang, Jie Gao, et al.
Journal of Thermal Science (2021) Vol. 30, Iss. 5, pp. 1674-1683
Closed Access | Times Cited: 6

Numerical Study on the Flow Mechanism of Compressor Rotor Blade Vibration under Different Inlet Probe Configurations
Rongfei Yang, Guoliang Wang, Haixu Liu, et al.
International Journal of Aerospace Engineering (2020) Vol. 2020, pp. 1-12
Open Access | Times Cited: 5

Numerical study of probe parameters on performance of a transonic axial compressor
Asad Islam, Hongwei Ma
PLoS ONE (2021) Vol. 16, Iss. 1, pp. e0245711-e0245711
Open Access | Times Cited: 5

Study on the influence of pneumatic probe on the wake flow field of transonic turbine cascade
Qingdian Zhang, Hongwei Ma, Anqi Xiao, et al.
Acta Mechanica Sinica (2024) Vol. 40, Iss. 7
Closed Access

Numerical Investigation of Probe-Support Intrusion Effects on Transonic Axial Compressor Performance
Asad Islam, Hongwei Ma
2022 19th International Bhurban Conference on Applied Sciences and Technology (IBCAST) (2020), pp. 459-466
Closed Access | Times Cited: 3

Effect of the distribution of the upstream probe support on performance of compressor cascade
Kuan-Xin Hou, Honghui Xiang, Jie Gao, et al.
International Journal of Turbo and Jet Engines (2022)
Closed Access

Accurate measurement and evaluation method of axial compressor efficiency under the influence of multiple factors
Yang Yong, Yaoming Fu, Binbin Lin, et al.
International Journal of Turbo and Jet Engines (2022) Vol. 40, Iss. s1, pp. s607-s619
Closed Access

Effect of the distribution of the upstream probe support on performance of compressor cascade
Kuan-Xin Hou, Honghui Xiang, Jie Gao, et al.
International Journal of Turbo and Jet Engines (2022) Vol. 40, Iss. s1, pp. s463-s473
Closed Access

Page 1

Scroll to top