相关期刊:《Theoretical & Applied Mechanics Letters》《Communications in Nonlinear Science and Numerical Simulation》《Journal of Physical Science and Application》《Energy Storage and Saving》更多>>
supported by the Science Center for Gas Turbine Project,China(No.P2022-B-II-020-001);the National Natural Science Foundation of China(No.52276123).
For the design and optimization of advanced aero-engines,the prohibitively computational resources required for numerical simulations pose a significant challenge,due to the extensive exploration of design parameters ...
supported by the National Natural Science Foundation of China(grant Nos.12272409,T2221002);Changsha Science and Technology Project(grant No.kq2107001);the Science and Technology Innovation Program of Hunan Province(grant No.2022RC1233);Hunan Provincial Innovation Foundation for Postgraduate(grant No.QL20230015).
The supersonic gas-particle two-phase transverse jet is a typical flow process in many applications,such as solid rocket scramjet.This study carried out experimental tests as well as Large Eddy Simulation(LES)to inves...
This project was supported by the Youth Independent Innovation Science Foundation of the Aerospace Technology Institute of China Aerodynamics Research and Development Center(Grant No.QNJJ23031).
The combustion performance of a scramjet engine is based on a two-phase mixing process of its fuel.To elucidate the mechanism of jet atomization in supersonic airflows,a numerical simulation of liquid jet atomization ...
supports from the National Natural Science Foundation of China(Nos.11902353,12272408,12102472,11902351,and 12102462);the National Science Fund for Distinguished Young Scholars,China(No.11925207);the Hunan Provincial Postgraduate Research Innovation Project,China(No.CX20210035).
The injection and atomization process of a liquid fuel jet is critical for an ignition start of a scramjet engine.Airwall-mounted crossflow injection strategy is widely used in scramjet combustors,avoiding high total ...
This work is supported by the National Natural Science Foundation of China(No.5212201273);the National Science and Technology Major Project of China(No.J2019-III-0003);The CFX software and computation resource supplied by Beijing Super Cloud Computing Center,China are acknowledged.
Rotor-stator cavities are frequently encountered in engineering applications such as gas turbine engines.They are usually subject to an external hot mainstream crossflow which in general is highly swirled under the ef...
supported by the National Natural Science Foundation of China (Grant Nos.12135008,12075150,and 12275174);the Shanghai Rising-Star Program (Grant No.22QA1404500);the Jingying Project of China National Nuclear Corporation。
Fuel assemblies have a decisive impact on the performance and safety of nuclear reactors.Helical fuel has huge potential for application in small module reactors(SMRs)due to its advantages in volume power density and ...
supported by the Khalifa Uni-versity under Awards No.CIRA-2018-051 and No.RCII-2019-003.
Increased power density in modern miniaturized electronics caused difficulty in keeping electronic performance effective.This challenge leads to the search for high-performance compact heat exchanger as one of the the...
supported by the National Natural Science Foundation of China(Nos.91641109 and 61827802)。
To study statistical characteristics of the random spray autoignition,aviation kerosene was injected transiently into non-vitiated air crossflow in a flow reactor with optical accesses.The operating conditions were re...
supported by the National Natural Science Foundation of China(Nos.91541203 and 51676204);the Fenglei Youth Innovation Fund of China Aerodynamics Research and Development Center(No.PJD20170186)。
This paper aims at probing the flow characteristics of a jet in supersonic crossflow(JISC)by installing a vortex generator(VG)upstream of the jet orifice.Nanoparticle planar laser scattering(NPLS)and stereo-particle i...
supported by the National Key Technology Research and Development Program of China(No.2016YFA0401200);the National Project for Research and Development of Major Scientific Instruments of China(No.11527802);the National Natural Science Foundation of China(Nos.91752102 and 11832018)。
An experimental study on the boundary layer transition over a delta wing was carried out at Mach number 6 in a quiet wind tunnel.The Nano-tracer-based Planar Laser Scattering(NPLS)and Temperature-Sensitive Paints(TSP)...