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

Getting to understand various parameters sensitivity

Wing Design Project for ENGR391 Fluid Mechanics

The aim of the project is to analyze and visualize the fluid flow condition over a wing structure under subsonic condition.

UNI project finding deflection of the wing with Finite element analysis

Extreme example of how long a split wing can hold air streamlines

To test the flow around NACA4415.
CFD.
To test the properties of the NACA4415.

To study flow around symmetric NACA airfoil.
CFD.
To study the wake downstream of a symmetric NACA airfoil.

This challenge is about designing your own lightweight design along with amazing renderings. The objective function is to reduce the weight of the wing without exceeding the maximum allowable deflection (+y direction) of 1 meter!

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.

Found an altoids box, a broken drone, and motors from an old DVD player and decided to try at making a glider to fly.

Structural Analysis of a UAV Wing with span of 4 meters

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.

Biplane wing separation analysis under high angle of attack

The purpose of this project is to study the influence of different types of winglets placed at the end of a commercial aircraft wing during takeoff. The flow will be considered incompressible and turbulent (kw-sst). The aerodynamic characteristics of the flow (lift, drag, eddies, etc.) will be determined.

This project involves meshing externally a Boeing 777-200 LR Aircraft, and then simulating its' operation on flight facing an airflow with an axial velocity of 50 m/s.  It is one of the longest-range commercial airliners, with an exterior length and wingspan reaching 63.70 and 64.80 meters respectively.  For this case a model with removed engines was chosen in order to assist convergence and meshing. Also a Symmetry plane was added midst the Part, and half the part was used for meshing and simulation for simplification.  A steady state compressible flow simulation is executed to visualize the air flow around the bodywork and wings of the aircraft, as well as the pressure distribution while on flight.

wing | SimScale Project Library | Page 4