supported by the National Key Project,China(No.GJXM92579);the Strategic Priority Research Program of Chinese Academy of Sciences,China(No.XDA17030100)。
Thermally-induced flow instabilities are a critical issue in multi-channel regenerative cooling systems.In particular,the interactions between Density-Wave Oscillations(DWO)and Flow Maldistribution(FMD)can result in c...
co-supported by the National Science and Technology Major Project of China (Nos. 2017-Ⅲ-00050029, J2019-Ⅲ-0021-0065, and J2019-Ⅲ-0015-0059);the National Natural Science Foundation of China (No. 51906009)
This study explores the design,analysis,and air pressure drop assessment of three analogous air–fuel heat exchangers consisting of thin serpentine tube bundles intended for use in high Mach number aero-engines.In hig...
primarily funded by the cooperative project offered by Beijing Key Laboratory of Space Thermal Control Technology;funded by China Postdoctoral Science Foundation(No.2020 M671618)。
The lunar surface is a typical vacuum environment,and its harsh heat rejection conditions bring great challenges to the thermal control technology of the exploration mission.In addition to the radiator,the sublimator ...
supported by the National Natural Science Foundation of China (No. 51676163);the National 111 Project, China (No. B18041;the Guangdong Basic and Applied Basic Research Foundation, China (No. 2019A1515111146)
Attempts for higher output power and thermal efficiency of gas turbines make the inlet temperature of turbine to be far beyond the material melting temperature.Therefore,to protect the airfoil in gas turbine from hot ...
supported by the National Natural Science Foundation of China (No. 51975471);Aviation Power Foundation of China (No. 6141B090319);Natural Science Basic Research Plan in Shaanxi Province of China (No.2018JM5173);National Natural Science Foundation of China(No. 51975471);National Science and Technology Major Project (2017-VIII-0003-0114);Natural Science Foundation of Shaanxi Province (No. 2018JQ5041)。
In this paper, the flow characteristics of the double wall structure are presented and the effect of the broken pin size on the cooling performance and flow field of the double wall configuration is investigated. A pe...
the financial support provided by the National Natural Science Foundation of China (No. 51475237);the National High-Tech Research and Development Program of China (No. 2013AA040101);the Program for New Century Excellent Talents in University (No. NCET-12-0627) of China;the Funding of Jiangsu Innovation Program for Graduate Education (No. KYLX_0232) of China
Nickel-based superalloys are widely employed in modern aircraft engines because of their excellent material characteristics, particularly in the fabrication of film cooling holes. However, the high machining requireme...
financial support provided by the National Natural Science Foundation of China(No.51475237);the National High-Tech Research and Development Program of China(2013AA040101);the Program for New Century Excellent Talents in University of China(No.NCET-12-0627);the Funding of Jiangsu Innovation Program for Graduate Education of China(No.KYLX_0232)
Single-crystal superalloys are typical advanced materials used for manufacturing aero- engine turbine blades. Their unique characteristics of high hardness and strength make them exceedingly difficult to machine. Howe...
support from Aeronautical Science Foundation of China(No.2011ZC09006)
Abstract This paper conducts a simulation study of a novel aircraft environmental control system based on membrane dehumidification (MD-ECS), and compares the system with the up-to-date four-wheel high pressure de-w...
supported by the National Natural Science Foundation of China (No. 51105024);National Science and Technology Major Project (No. 2013ZX04001051)
The effectiveness of grinding fluid supply has a crucial impact on grinding quality and efficiency in high speed grinding. In order to improve the cooling and lubrication, through in-depth research of self-inhaling in...
supported by the National Natural Science Foundation of China (Grant No.: 50976008)
An experimental investigation is conducted to obtain the heat transfer and pressure drop data for an integral trailing edge cavity test section that simulates a novel turbine blade's internal cooling passage with ble...