Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Jixin XIANG"'
Publikováno v:
Aerospace, Vol 11, Iss 6, p 433 (2024)
To investigate the wall cooling of the thrust chamber in an engine, two film-cooling structures, namely, a circular hole structure and a slot structure, were designed. Numerical simulations were performed to study the coupled flow and regenerative co
Externí odkaz:
https://doaj.org/article/7d6c08eb28ed41a58733e0b382cca2c5
Publikováno v:
Taiyuan Ligong Daxue xuebao, Vol 53, Iss 4, Pp 751-758 (2022)
To meet the design requirements of long-endurance hydrogen energy hybrid powered Unmanned Aerial Vehicle, the combined MATLAB and XFOIL optimization methods, based on the optimized airfoil, were used to optimize the design of the airfoil of HM114. Tw
Externí odkaz:
https://doaj.org/article/110239b0ad8144e79736bfc19ce39a81
Publikováno v:
Aerospace, Vol 10, Iss 5, p 484 (2023)
The buckling failure of the afterburner cylinder is a serious safety concern for aero-engines. To tackle this issue, the buckling simulation analysis of the afterburner cylinder was carried out by using finite element method (FEM) software to obtain
Externí odkaz:
https://doaj.org/article/0a82d9b79d964f1b9b2624aa2f9bf1b1
Autor:
Jixin XIANG, Bing SUN
Publikováno v:
Journal of Thermal Science and Technology, Vol 13, Iss 2, Pp JTST0035-JTST0035 (2018)
To better understand the performance of gaseous film cooling near the injector region in the LOX/GH2 thrust chambers, a methodology is employed to simulate the coupled heat transfer of the film cooling in thrust chambers with regenerative cooling. Th
Externí odkaz:
https://doaj.org/article/384194c74dd04bcc9941ad3b87d35ee2
Publikováno v:
Journal of Thermal Science and Technology, Vol 13, Iss 1, Pp JTST0016-JTST0016 (2018)
In order to understand heat transfer mechanisms in the combustion chamber with multi-elements injector and provide benchmark data of wall heat fluxes for the CFD code validation, experiments were carried out in a GH2/GO2 heat-sink combustion chamber.
Externí odkaz:
https://doaj.org/article/44dcdc3550454ca1a799e2f4a90c16f6
Publikováno v:
Applied Thermal Engineering. 138:913-923
Heat transfer management of the combustion chamber walls of rocket engines is key to predicting their life-cycle. This study used a test apparatus to measure heat transfer on the inner wall of a film-cooled combustion chamber. Experiments on a heat-s
Publikováno v:
Soft Matter. 8:765-773
It is well-known that the phenylboronic acid derivatives have chemical interactions with sugars. Hence, stable nanoparticles with core-shell structure were formed by the covalent complexation between boronic acid groups of poly(3-acrylamidophenylboro
Publikováno v:
Journal of Thermal Science and Technology. 13:JTST0016-JTST0016