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This simulation aims to study the aerodynamic of the tesla cybertruck.

Here I will make the pressure and speed gradient around the airfoil of the aircraft.

Simulation of the aerodinamics of a model rocket

The Lockheed Martin RQ-170 Sentinel is an American unmanned aerial vehicle (UAV) developed by Lockheed Martin and operated by the United States Air Force for the Central Intelligence Agency (CIA). It's curious to note that its aerodynamic profile resembles that of a peregrine falcon. There's not much information about this aircraft, but it's estimated that it can reach a speed of 950 km/h and 1400 km of autonomy. Which's the secret to reach a high velocity is the project goal. The drag coefficient is a good reason for this. In this project, we can calculate the drag coefficient using an Incompressible Flow solver.

Design and Analysis of Spur Gear for Dynamic Applications

Barnouli principle. 
How to produce lift force.

space one day is my dreams elon musk is my hero/role model

External Flow simulation of unmanned aerial vehicle

Analysis of the engines heat transfer for design of the cooling system

To look over the flow of air through a Ramjet engine.

Trial No. 3 to check the Mechanics of the parachute

I want to learn more about the design aspects of the parachute for the Rockets and all. So here it is. Please Chuck it, the speeds are not at all realistic.

Flow Analysis Over Alfa Romeo QV without any aerodynamic aids.

to find which model is best for a blended wing body plane, fluid dynamics, it is for a project

Lift test on propeller blade to determine which propeller would be the most efficient

testing my seat for class
For Aerospace class

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.

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.

Trying to simulate wether the design will work making a mini jet engine irl

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

This project  involves meshing a single-Shaft Turbofan Engine, and then simulating its' operation when facing an axial airflow of 150 m/s, while rotating with a velocity of 940 rad/sec (9000 rpm) . A Fan is used to bypass a large amount of air in the inside of the engine. For this case the typical Compressor, Combustion chamber and Turbine Stator were omitted, and only the Fan, Shaft, Shell and Turbine rotor were meshed and examined, in order to restrain the meshing requirements for complex, time consuming meshing and simulation.  A steady state incompressible flow simulation is executed to visualize the air flow through the components of the Turbofan, as well as the pressure and U magnitude distribution on the blades of the Fan and Turbine.

Link to  the extended compressible study (bigger domain included) : https://www.simscale.com/projects/fsite/turbofan_engine_extended_study/

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