Rui Zhang

Prof. Dr. Rui Zhang

School of Aeronautics and Astronautics, Central South University, Changsha, Hunan, China
+2
orcid

Research Focus & Metrics

Academic Career Length

15Years (2012-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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1 December 2013 in Review of Scientific Instruments
Verified
Journal Article
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DZDaixian Zhang
Daixian Zhang
JWJianjun Wu
Jianjun Wu
RZRui Zhang
Rui Zhang
HZHua Zhang
Hua Zhang
ZHZhen He
Zhen He
A sympathetic resonance theory is analyzed and applied in a newly developed torsional pendulum to measure the micro-impulse produced by a μN s-class ablative pulsed plasma thruster. According to theoretical analysis on the dynamical behaviors of a torsional pendulum, the resonance amplification effect of micro-signals is presented. In addition, a new micro-impulse measurement method based on sympathetic resonance theory is proposed as an improvement of the original single pulse measurement method. In contrast with the single pulse measurement method, the advantages of sympathetic resonance method are significant. First, because of the magnification of vibration signals due to resonance processes, measurement precision for the sympathetic resonance method becomes higher especially in reducing reading error. With an increase in peak number, the relative errors induced by readout of voltage signals decrease to approximately ±1.9% for the sympathetic resonance mode, whereas the relative error in single pulse mode is estimated as ±13.4%. Besides, by using the resonance amplification effect the sympathetic resonance method makes it possible to measure an extremely low-impulse beyond the resolution of a thrust stand without redesigning or purchasing a new one. Moreover, because of the simple operational principle and structure the sympathetic resonance method is much more convenient and inexpensive to be implemented than other high-precision methods. Finally, the sympathetic resonance measurement method can also be applied in other thrust stands to improve further the ability to measure the low-impulse bits.

1 April 2013 in Applied Surface Science
Verified
Journal Article
Closed access
RZRui Zhang
Rui Zhang
DZDaixian Zhang
Daixian Zhang
FZFan Zhang
Fan Zhang
ZHZhen He
Zhen He
JWJianjun Wu
Jianjun Wu

7 February 2023 in International Journal of Computational Fluid Dynamics
Verified
Journal Article
Closed access
JZJianbo Zhou
Jianbo Zhou
RZRui Zhang
Rui Zhang
LCLyu Chen
Lyu Chen

24 February 2024 in Processes
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Journal Article
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JZJianbo Zhou
Jianbo Zhou
LCLyu Chen
Lyu Chen
RZRui Zhang
Rui Zhang
WZWeidong Zhao
Weidong Zhao
In the pursuit of understanding the oxidation mechanisms of hydrogenated biodiesel fuels and elucidating the combustion behavior of biomass fuels when blended with diesel, this study presents a comprehensive investigation into the reaction mechanism of hydrogenated biodiesel–ethanol–diesel mixtures. We develop a comprehensive reaction mechanism encompassing 187 components and 735 reactions for hydrogenated biodiesel–ethanol–diesel mixtures. Through kinetics analysis under varied conditions, including 1.0 MPa pressure, an equivalence ratio of 1.0, and temperatures of 900 K and 1400 K, we explore the impact of cross-reactions and changing fuel blend ratios on low- and high-temperature oxidation. Our findings indicate that oleic and stearic acid methyl esters serve as better substitutes for representing hydrogenated biodiesel kinetics than methyl decanoate. At lower temperatures, increased hydrogenated biodiesel and ethanol content leads to reduced OH generation, impacting reactivity. Conversely, higher temperatures result in enhanced OH production with increased hydrogenated biodiesel and ethanol concentrations, promoting reactivity. A cross-reaction analysis reveals CH2O as a prominent product, with the CH2O→HCO→CO pathway playing a pivotal role. In summary, our research unveils the intricate oxidation mechanisms of hydrogenated biodiesel–ethanol–diesel mixtures, providing insights into their combustion characteristics and offering implications for optimizing fuel blends for cleaner and more efficient energy solutions.

16 November 2023 in Materials Today Communications
Verified
Journal Article
Closed access
JZJianbo Zhou
Jianbo Zhou
DHDongjing He
Dongjing He
RZRui Zhang
Rui Zhang

24 October 2023 in Processes
Verified
Journal Article
Open access
PDF file
JZJianbo Zhou
Jianbo Zhou
DHDongjing He
Dongjing He
RZRui Zhang
Rui Zhang
WZWeidong Zhao
Weidong Zhao
The performance of centrifugal aviation fuel pumps can be crucial in determining aircraft efficiency and safety. Here, we delve into the intricate interplay between flight altitude and flow rate on pump performance. Employing the central composite design method, we characterized the relationship between these parameters and the pump’s head and efficiency. Our analysis, underpinned by response surface methodology, revealed distinct optimal operating conditions at 10,000 m and 12,000 m flight altitudes, pinpointed at flow rates of 1.1016 Q and 1.1222 Q, respectively. Moreover, the emergence and growth of cavitation regions with increasing flow rates underscore the challenges in pump operation. Significantly, we identify rotor–stator interactions as a dominant influence on pressure fluctuations, especially near the impeller exit. These findings not only elucidate the operational dynamics of aviation fuel pumps but also pave the way for advanced pump designs and optimizations.