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Looking to achieve a smooth airfoil from a csv file imported into Fusion 360 and transfer into STL format, so I get a smooth model in Simscale, as the delete feature in the Flow region cannot create a smooth surface

The goal is to test the temp and pressure of wings

analyzing a random wing to start simscale

a airplane wing without body of aircraft or engines

Aerodynamic of an electric stealth drone.

A simulation work to validate the wind tunnel experiment with GA (W) - 2 airfoil.

The full published research article of this project is available at: https://doi.org/10.46873/2300-3960.1063

First test of the airfoil for an engine
Aim to speed up the air

Just trying CFD for the first time on a wingtip I designed for my RC airplane.

To Calculate Thrust and Drag on the NACA 4412 Airfoil

The aim of this project is to study the influence of rear wing support position. In particular, in this CFD simulation a low side support rear wing will be studied.

The aim of this project is to study the influence of rear wing support position.
In particular, in this CFD simulation a high side support rear wing will be studied.

KFm3 Airfoil CFD Simulation for use on remote controlled aircraft.

A shingle designed like a reverse upper layer airfoil, adding an aerodynamic shape lowering both wind pressure, and long term damage to shingles.

The goal is to investigate the behavior of an one-hour-design 3D printed glider while it gets actually printed.

116 minutes remaining before the wing sections are printed. Fin and fuselage still needs to be manufactured.
Hopefully some useful information will be acquired from this steady state incompressible CFD simulation before the hardware is all ready.
What is the speed range this plane can operate. Will this plane actually fly or it will be just a demo piece.

The glider is designed by some rules of thumb. 

Progress in the comments below!

NACA 0012 airfoil from NASA's TMR website.

In this project we examined the Effect of Boundary Layers on the  NACA 0012 Airfoil. In-compressible fluid flow simulation is selected for the project. Free stream velocity is selected as 10 m/s having A.O.A  10 with the airfoil.

This project important point of video shooting and very impressive photos click by drones camera

In this project steady state incompressible fluid flow simulation of a small RC aircraft is performed for the completion of aircraft design course on SimScale's Academy. Two simulation at different AOA relative to wing is carried out to obtain the coefficient of lift and drag. Lift and drag forces are calculated at 3 and 20 AOA, also the flow around the aircraft is also visualized for the design consideration.

airfoil | SimScale Project Library | Page 2