Zobrazeno 1 - 10
of 77
pro vyhledávání: '"Zhenbing Luo"'
Publikováno v:
Advances in Aerodynamics, Vol 5, Iss 1, Pp 1-23 (2023)
Abstract Turbulence drag reduction is of great significance for the range increase of hypersonic flight vehicles. The proposed velocity-temperature coupling control method (Liu et al, Phys Rev Fluids 6:044603, 2021) is further extended to the hyperso
Externí odkaz:
https://doaj.org/article/c24955db41db47d8b28b48f5ad565e6a
Publikováno v:
Aerospace, Vol 10, Iss 9, p 766 (2023)
Transition delaying is of great importance for the drag and heat flux reduction of hypersonic flight vehicles. The first mode, with low frequency, and the second mode, with high frequency, exist simultaneously during the transition through the hypers
Externí odkaz:
https://doaj.org/article/180c1596ee774ff5bac7673f5479313e
Publikováno v:
Actuators, Vol 12, Iss 6, p 250 (2023)
With the aim of increasing the momentum jet and obtaining better environmental adaptability, this study designs a new type of actuator combining a sparkjet actuator and a combustion-driven actuator. Numerical simulation shows that the combustion-driv
Externí odkaz:
https://doaj.org/article/2ff8cc824ed9481088ef2912e5fcfeb2
Publikováno v:
Actuators, Vol 11, Iss 12, p 376 (2022)
In order to understand the impingement flow field and cooling characteristics of vectoring dual synthetic jets (DSJ), an experimental investigation was performed to analyze the parameter effects. With the variation of the slot location, the vectoring
Externí odkaz:
https://doaj.org/article/6659d2a0ab6a488f9d763c7fe9c28b97
Publikováno v:
Actuators, Vol 11, Iss 12, p 382 (2022)
Increasing heat flux restricts the development of the miniaturization of electronic devices. There is an urgent need for a heat dissipation method that will efficiently cool the chip. This paper presents a novel liquid cooling device based on dual sy
Externí odkaz:
https://doaj.org/article/52215ad4127f4fef8c93f71f48fbd24c
Autor:
Yinxin Zhu, Zhenbing Luo, Wenqiang Peng, Qiang Liu, Yan Zhou, Wei Xie, Pan Cheng, Zhengxue Ma, Xuzhen Xie
Publikováno v:
Aerospace, Vol 9, Iss 11, p 713 (2022)
To effectively reduce shock wave loss at the trailing edge of a supersonic cascade under high back-pressure, a shock wave control method based on air jets is proposed. The air jet was arranged on the pressure side of the blade in the upstream of the
Externí odkaz:
https://doaj.org/article/22e482f38ab74295bd9a9a5c8bd29d8d
Publikováno v:
Actuators, Vol 11, Iss 8, p 205 (2022)
In order to understand the differences between dual synthetic jets (DSJs) and synthetic jets (SJs), particle image velocimetry (PIV) technology is used to capture the basic flow field characteristics of a dual synthetic jet actuator (DSJA) and a synt
Externí odkaz:
https://doaj.org/article/219794356ed2435d99cf29ed50857787
Publikováno v:
Chemical Engineering Transactions, Vol 81 (2020)
The effect of impingement cooling using a dual synthetic jet actuator (SJA) with improvement of exit configuration has been investigated experimentally. A hump with cross section of a half-elliptic shape was attached to the flat between the two exits
Externí odkaz:
https://doaj.org/article/76a07043a5954da790996bb26819b203
Autor:
Wei Xie, Zhenbing Luo, Yan Zhou, Xuzhen Xie, Jianjun Wu, Guanghui Bai, Zheng Li, Hao Dong, Xudong Zhang
Publikováno v:
AIAA Journal. 61:1428-1434
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::13eaf4cf1b904febae15232a757efe55
https://doi.org/10.2514/1.j062580
https://doi.org/10.2514/1.j062580
Autor:
Binghai Sun, Zhenbing Luo, Xiaoyu Zhu, Yuting Shao, Wenhai Zhang, Guihua Qin, Shuwei Lin, Simin Wan
Publikováno v:
Experimental Aging Research. :1-23
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e3071e9415a980ddc6fefafc41d57cf3
https://doi.org/10.1080/0361073x.2023.2168990
https://doi.org/10.1080/0361073x.2023.2168990