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basic aerodynamic simulation of the model planne

Experiments and comparaison of different single seater step planes at 180 km/h (50 m/s). I use a quickly made sort of single seater design.
Results :
Reference (no step plane)              : 1740 N of drag, 330 N of lift.
Flat step plane                                      : 1793 N of drag, 255 N of lift.
Flat step pland and side skirts     : 1800 N of drag, 55N of lift.
Flat step pland and all skirts         : 2025 N of drag, 650 N of lift.
Flat round step plane with skirt : 1880 N of drag, 760 N of downforce.
Angled step plane                               : 1840 N of drag, 450 N of downforce.
Angled step plane with skirts      : 1850 N of drag, 620 N of downforce.

In this simulation, it is aimed to calculate the drag coefficient of an experimental rocket. Although the rocket geometry used is representative, the drag coefficient can be calculated for realistic models by following the simulation steps. K-w SST turbulence model was used for simulation. For the experimental rocket, the speed was taken 270 m / s and a ninety-degree (not realistic) flight angle assumption was made.

To increase aerodynamic efficiency with the help of leading edge slot. A passive flow control technique

This project contains resources for Session 1 of the F1 Workshop

This project simulates the airflow around an approximative model of the newly announced Tesla Cybertruck

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

To simulate the external aerodynamics of a fighter plane

The rear wing plays a vital role to maintain the friction on the ground. The simulation analysis a flow over a rear wing developed to study the airflow patterns. An incompressible  external flow analysis is carried out to determine its flow patterns.

analise para aprender a utilizar o software a fim de simular o comportamento de stall da asa

Es una prueba del modelo de porosidad en un muffler

In thise simulation i want to show how importent a endplate is one a rearwing.

Simulating Toothless from 'How to train your dragon' flying in air. 

First project here, so Toothless is incomplete and I'll probably make some mistakes regarding the simulation parameters and such

As part of my 3rd year MEC307 - Group Design project at the University of Sheffield
Looking into the effects of DRS on SFR11.
This is a baseline sim to compare the rear wing in its closed state and with all the flaps open when pivoted at 50 percent cord length.
The sim is for the REAR WING ONLY. This is to reduce computing power as a basline to see how much drag is reduced by in order to complete preliminary lap time simulations. 
Original investigations on the lap sim showed that a DRS system that reduced drag by 50 percent could reduce autocross times by 0.2 seconds with an overall dynamic events bonus of 6.5 points.

my plan for this simulation is to use a 3d model that I have already created of a fighter jet and run it through some aerodynamics simulations. hope you enjoy :-)

does having cargo onboard a freighter slow it down in respect to air resistance(question mark) now you know.

this project is dedicated to investigating the drag effect on a special type of aircraft's tail, in order to test its aerodynamic efficiency.

Experimenting with aerodynami aspect of Truck shape

aerodynamics | SimScale Project Library | Page 86