Maochao Xiao

Maochao Xiao

PhD student

Sapienza University of Rome

Biography

Maochao Xiao is a PhD student in Aeronautics and Space Engineering at Sapienza University of Rome. He shows interest in exploiting machine learning for turbulence modeling in large eddy simulation (LES) and Reynolds-averaged Navier-Stokes (RANS), while leveraging graphics processing units (GPUs) for computational efficiency. His recent activities focus on the development of robust wall models for large-eddy simulation based on reinforcement learning (RL).

Interests
  • Computational Fluid Dynamics
  • Machine Learning
  • GPU Acceleration
Education
  • PhD in Aeronautics and Space Engineering, 2025

    Sapienza University of Rome

  • MEng in Aeronautical and Astronautical Science and Technology, 2019

    Tsinghua University

  • B.Eng. in Flight Vehicle Propulsion Engineering, 2016

    Northwestern Polytechnical University

Projects

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Detached-Eddy Simulation
A shear-layer-adapted subgrid length scale is applied to improved delayed detached eddy simulation to alleviate the “grey area” issue, and an anisotropic-minimum-dissipation subgrid length scale is further proposed to enhance the computational accuracy on anisotropic meshes.
Detached-Eddy Simulation
Drag Reduction in Rotating Pipe Flow
Direct numerical simulations are performed to investigate the drag reduction and near-wall coherent structures in rotating pipe flow up to Re𝜏 ≈ 3000
Drag Reduction in Rotating Pipe Flow
Iced-Wing Aerodynamics
Scale-resolving simulations are conducted to unveil the separated flow around iced wings and iced high-lift configurations.
Iced-Wing Aerodynamics

Codes

CFL3D-enhanced
CFL3D-enhanced features hybrid RANS/LES simulation, leveraging an anisotropic minimum-dissipation IDDES model (AMD-IDDES). Inviscid flux scheme is a blended central/upwind scheme. Enhanced I/O capabilities include flow field averaging, animating and sampling. The modified version is available on request. Please check the author’s GitHub for more open-source codes.
CaNS
CaNS (Canonical Navier-Stokes) is a code for massively-parallel numerical simulations of fluid flows. It aims at solving any fluid flow of an incompressible, Newtonian fluid that can benefit from a FFT-based solver for the second-order finite-difference Poisson equation in a 3D Cartesian grid.
STREAmS-2
STREAmS (Supersonic TuRbulEnt Accelerated navier–stokes Solver) performs Direct Numerical Simulations of compressible turbulent flows in Cartesian geometry solving the unsteady, fully compressible Navier-Stokes equations for a perfect gas.