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寻找受海浪影响最小的浮台形状

This project analyzes the aerodynamic performance of an airfoil under high-speed airflow conditions using Computational Fluid Dynamics (CFD). The airfoil is subjected to a velocity of 75 m/s to simulate realistic conditions for aerospace and wind energy applications. The analysis focuses on evaluating pressure distribution, velocity fields, and lift and drag forces to optimize airfoil efficiency and stability. The simulation uses the incompressible flow model with the k-ω SST turbulence model to capture boundary layer behavior accurately.

CFD exercise 3 from UCSC RT CFD Onboarding

Senior Design Project calculation for drag coefficients

fornt wing sim - Copy - Copy - Copy - Copy

To check flow rate of PVA Glue through nozzle for direct application

Two-dimensional laminar flow past a circular cylinder

CFD Validation of Individual  Aerodynamic Components as well  wind tunnel sections

étudo de transference chaleur pour module Peltier

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