sponsored by the National Natural Science Foundation of China(No.51906207,No.U22B2091);the Young Elite Scientists Sponsorship Program by CAST(2021QNRC001);Technical Field Foundation(2021-JCJQ-JJ-0342)。
SCRamjet is exposed to severe thermal environments during hypersonic flights,which poses a serious challenge to the engine cooling technology.Regenerative cooling with hydrocarbon fuel is considered promising,in which...
supported by the National Natural Science Foundation of China(Grant No.52076088);the National Key Research and Development Program of China(Grant No.2022YFB4003801).
To enhance the cooling capacity of traditional microchannels for high heat flux electronic devices,a microchannel design with staggered semi-elliptical ribs is proposed in this paper.Through numerical simulations,the ...
supported by the Structures and Materials(S&M)Research Lab of Prince Sultan University;support of Prince Sultan University in paying the article processing charges(APC)for this publication.
When better fuel-air mixing in the combustion chamber or a reduction in base drag are required in vehicles,rockets,and aeroplanes,the base pressure control is activated.Controlling the base pressure and drag is necess...
This study deals with base pressure management in a duct for various values of the Mach number(M),namely,Mach number corresponding to sonic and four supersonic conditions.In addition to the Mach number,the nozzle pres...
carried out in the framework of AIRGREEN2 Project,which gratefully received funding from the Clean Sky 2 Joint Undertaking,under the European’s Union Horizon 2020 Research and Innovation Program,Grant Agreement(No.807089—REG GAM 4822018—H2020-IBA-CS2-GAMS-2017);funded by TUBITAK 2214-A-International Research Fellowship Programme for Ph.D.Students。
The design and application of morphing systems are ongoing issues compelling the aviation industry.The Clean Sky-program represents the most significant aeronautical research ever launched in Europe on advanced techno...
the National Natural Science Foundation of China(No.U2037204);the 111 Project(B17034);Innovative Research Team Development Program of Ministry of Education of China(No.IRT17R83);the National Natural Science Foundation of China(No.52005375)for the support given to this research。
Cylindrical rings with thin wall and high web ribs(CRTWHWR)are widely used as the key load bearing structures such as rocket body and space station cabin in aerospace field.However,it is still difficult to efficiently...
supported by discipline construction fund of Tsinghua University。
To deal with the aerodynamic heating on the aircraft surface,a potential solution is to utilize liquid cooling via the channels in part of the fuselage.This is a typical problem of flow and heat transfer in channels w...
the National Natural Science Foundation of China (No. U2037204);the 111 Project (No. B17034);Innovative Research Team Development Program of Ministry of Education of China (No. IRT17R83);the National Natural Science Foundation of China (No. 52005375)
Tapered ring with thin wall and three high ribs(TRTWTHR),showing complicated geometry(wall thickness is less than 4 mm and rib height exceeds 20 mm),is extensively utilized to fabricate the critical structural parts o...
co-supported by the National Natural Science Foundation of China(No.52075501);the Fundamental Research Program of Shanxi Province,China(No.20210302124206).
The Large-size Conical Cylinders with Inner Transverse High Ribs(LCCWITHR) can reduce the weight of the parts while maintaining high rigidity and strength. Radially Loading Rotary Extrusion(RLRE) forming technology ca...
supported by King Mongkut’s Institute of Technology Ladkrabang [2566-02-01-006].
Simulation of fluid-flow topology and thermal behavior in a round tube heat exchanger(RTHX)installed by three V-rib sets is reported.The expected phenomena for the rib installation are the generated vortex flow,imping...