Zobrazeno 1 - 10
of 92
pro vyhledávání: '"Yuanjun Zhang"'
Publikováno v:
Frontiers in Psychiatry, Vol 15 (2024)
BackgroundAlthough impaired auditory mismatch negativity (MMN) has consistently been found in individuals with schizophrenia, there are few and inconsistent reports on nonclinical individuals with schizotypy. To date, no studies have thoroughly asses
Externí odkaz:
https://doaj.org/article/f857741bd97042e2b641da4077dce20b
Autor:
Yuanjun Zhang, Dong Wu, Maojie Liao, Xuewen Shi, Feng Chen, Chengguang Zhang, Ming Cai, Jun Tang
Publikováno v:
Geofluids, Vol 2024 (2024)
Horizontal wells are extensively utilized in the development of unconventional reservoirs. However, the logging responses and formation evaluation in horizontal wells can be impacted by factors like anisotropy and tool eccentricity. To investigate th
Externí odkaz:
https://doaj.org/article/1b55dfa3b864455497eb8e345c32b676
Publikováno v:
Frontiers in Human Neuroscience, Vol 17 (2023)
BackgroundThe aim of this study was to compare the characteristics of auditory P300 between non-clinical individuals with high and low schizotypal traits, and investigate the relationship between schizotypy and P300 under various oddball conditions.M
Externí odkaz:
https://doaj.org/article/7e3c4db649144c679bae751abdcce49b
Publikováno v:
Frontiers in Materials, Vol 9 (2022)
Acoustic metasurfaces have been increasingly explored in the past 10 years because of their compact structure and wave manipulation capabilities. In this work, we explore the feasibility of using an acoustic metasurface lens (MSL) for the characteriz
Externí odkaz:
https://doaj.org/article/baa4f7324b65410bad9adf13f56f7a78
Autor:
Guanyao Wang, Ming Zhu, Ying Zhang, Chan Song, Xiaolong Zhu, Zhongyi Huang, Yuanjun Zhang, Fangfang Yu, Gang Xu, Minghong Wu, Hua‐Kun Liu, Shi‐Xue Dou, Chao Wu
Publikováno v:
InfoMat, Vol 4, Iss 7, Pp n/a-n/a (2022)
Abstract The undesirable Li dendrite growth and other knock‐on issues have significantly plagued the application of Li metal anodes (LMAs). Herein, we report that the synergistic regulation of double interfaces adjacent to the metallic Li anode can
Externí odkaz:
https://doaj.org/article/38bb327d23844d728435251cd8f8296f
Publikováno v:
Aerospace, Vol 10, Iss 5, p 440 (2023)
This study investigated reconstruction techniques for building the instantaneous fuel regression rate of the hybrid rocket motor (HRM). Specifically, an experiment in a laboratory 500 N-class hybrid rocket motor with single-port wagon wheel fuel grai
Externí odkaz:
https://doaj.org/article/2efbf2f16df042ec803bd9e678a16c02
Publikováno v:
Aerospace, Vol 10, Iss 5, p 421 (2023)
Space exploration greatly facilitates the development of advanced propulsion systems. Extensive research has shown that hybrid rocket motors have bright prospects for use in variable-thrust propulsion systems. However, the variable-thrust precision c
Externí odkaz:
https://doaj.org/article/723996d60e5541b180da2651f70918d0
Autor:
Lin Chen, Wenkang Zou, Jihao Jiang, Liangji Zhou, Bing Wei, Fan Guo, An He, Weiping Xie, Jianjun Deng, Meng Wang, Jie Wang, Yuanjun Zhang
Publikováno v:
Matter and Radiation at Extremes, Vol 6, Iss 4, Pp 045901-045901-6 (2021)
In this paper, the results of tests on a 0.76-TW linear transformer driver (LTD) module for Z-pinch research are presented for the first time. Ten LTD cavities, each generating a 1-MA/90-kV pulse on a matched load, were connected in series with a mag
Externí odkaz:
https://doaj.org/article/8ee8ae733b4342db8d60598db53be991
Design Optimization and Parameter Analysis of a Hybrid Rocket Motor-Powered Small LEO Launch Vehicle
Publikováno v:
International Journal of Aerospace Engineering, Vol 2021 (2021)
In this paper, the effects of different grain shapes of a hybrid rocket motor (HRM) and different payload mass/orbit heights on the design of small launch vehicles (SLVs) are systematically discussed. An integrated overall design model for the hybrid
Externí odkaz:
https://doaj.org/article/6ba0f870489b47e0834c1014a76a5ee0
Experimental and Numerical Investigations on the Ignition of RBCC Gas-Oxygen/Kerosene Rocket Ejector
Publikováno v:
International Journal of Aerospace Engineering, Vol 2021 (2021)
The rocket ejector refers to a core component of a rocket-based combined cycle (RBCC) engine. The ignition is of critical significance for rocket ejection. Reliable and stable ignition crucially determines the normal operation of the engine. In this
Externí odkaz:
https://doaj.org/article/b1f3209b286e46309b1492519a916a67