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Fax: 86-24-86520827

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AVICARI developed its own aeronautical numerical simulation platform ARI_CFD, which contains many functional modules, such as low order panel method module, high order panel method module, Cartesian grid high speed aerodynamic analysis module based on Euler equation, structured grid module, unstructured grid module, unstructured dynamic overset grid module and hypersonic specialized module. ARI_CFD platform can satisfy CFD simulation requirements of different levels and velocity ranges, from fast evaluation in conceptual design phase to accurate analysis in detailed layout scheme fine design phase, as well as from subsonic to hypersonic flow, for aircraft, high-speed rail and automobile. Depending on ARI_CFD platform, AVICARI has formed high efficiency conventional engineering simulation and multiple special simulation technologies, including hybrid RANS/LES simulation, transition prediction, weapon jettison simulation, numerical simulation of slipstream for rotor-wing propeller, aero-elastic numerical simulation, hypersonic numerical simulation, icing numerical simulation and aerodynamic noise simulation.

AVICARI is capable of CFD platform development, conventional engineering application & validation and special simulation technology study, being able to provide customers with aerodynamic technical problem resolution in products developing.

Conventional Engineering Application and Validation

Hybrid RANS/LES Simulation

Transition Prediction

Weapon Jettison Simulation

Numerical Simulation of Slipstream for Rotor-wing Propeller

Aero-elastic Numerical Simulation

Hypersonic Numerical Simulation

Icing Numerical Simulation

Aerodynamic Noise Simulation