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High-Fidelity Computational Aerodynamics of the Elytron 4S UAV

机译:Elytron 4S UAV的高保真计算空气动力学

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High-fidelity Computational Fluid Dynamics (CFD) have been carried out for the Elytron 4S Unmanned Aerial Vehicle (UAV), also known as the converticopter "proto12". It is the scaled wind tunnel model of the Elytron 4S, an Urban Air Mobility (UAM) concept, a tilt-wing, box-wing rotorcraft capable of Vertical Take-Off and Landing (VTOL). The three-dimensional unsteady Navier-Stokes equations are solved on overset grids employing high-order accurate schemes, dual-time stepping, and a hybrid turbulence model using NASA's CFD code OVERFLOW. The Elytron 4S UAV has been simulated in airplane mode and in helicopter mode.
机译:为Elytron 4s无人机(UAV)进行了高保真计算流体动力学(CFD),也称为转换机“PROTO12”。它是Elytron 4s的缩放风洞模型,一种城市空移(UAM)概念,倾斜翼,箱翼旋翼飞机,能够垂直起飞和着陆(VTOL)。通过使用NASA的CFD码溢出,使用高阶准确方案,双时踏步和混合湍流模型的潜推网格解决了三维非稳态Navier-Stokes方程。 Elytron 4S UAV已在飞机模式和直升机模式下模拟。

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