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Mao-lab

Mao-labMao-labMao-lab
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Simulation of high-speed fluid flow around a cylindrical object with Mach, temperature, and pressure gradients.

HYbrid CPU-GPU Variable-order Element-based compressible flow Solver

HYVES, a high-fidelity compressible flow solver for complex geometries that leverages the variable-order and element locality properties of the Flux Reconstruction method to achieve high performance on heterogeneous computing architectures.

Login page for a data fusion and prediction software.

RapidFlow-DF

A Flow Field Data Fusion and Rapid Forecasting System, for multi-source and multi-fidelity data fusion, reduced-order modeling, an d rapid prediction of unsteady flow fields.

IceCrystalFOAM

For predicting ice crystal transport, phase change, particle-wall interaction and icing at aeroengine conditions.

3D visualization of fluid dynamics with velocity and vorticity gradients.

HypHaar solver

For solving hypersonic compressible flows using the Haar wavelet collocation method, delivering exceptional stability across strong shock waves for critical aerospace aerodynamic.

Close-up of a microscope in a laboratory setting.

N3D

For direct numerical simulation (DNS), linear stability analysis, and adjoint-based optimization of incompressible flows via spectral-element/Fourier discretization and velocity-correction projection on complex geometries in parallel.

Metal sensor box with attached cable on white background.

Three-Component Strain-gauge Balance

This three-component strain-gauge balance is used to measure the aerodynamic forces in wind tunnels. The maximum measurement force is 50N.


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