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Modelling the unpropelled glide phase of a re-usable first stage using the RFZ model, an open source geometry similar to Falcon 9

Experiment with small micro channel compressible and incompressible flow.

supersonic compressible flow with suction phenomena on secondary inlet

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.

How was advanced the the horten 229 aerodynamic

Check out www.simscale-academy.com for more classes on simulation.

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.

An air flow bench is a device used for testing the internal aerodynamic qualities of an engine component and is used primarily for testing the intake and exhaust ports of cylinder heads of internal combustion engines, but the cost of flow bench is very high and thus, with the advent in computational simulation technology the port flow simulation can be conducted very easily to analyse the breathing capacity of the engine.

As a follow-up case for the  TurboFan engine case: https://www.simscale.com/projects/fsite/new_jet/, this project extends the study by using a compressible flow simulation.  It 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  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.

The project goal is to determine the effect of diameter and length design on speed of the air while passing through the nozzle.
Compressible flow CFD analysis will be run to determine the flow speed and pressure drop.
This system are being used in agriculture projects. The system pushes the air with a specific speed to wet the specific area with specific drop value in micron levels. The air carry water , drug sprinkles up to 100 meters and make it easy to wet and disinfection the area.

A chemically reacting fluid flows through a channel.Design considerations require that the flow area of the duct be abruptly
reduced to 1/10th of its size. To prevent destruction of the duct by the reacting fluid,no stagnant eddies at the contraction can be allowed.have some control over the duct length upstream of the contraction, and thus the velocity profile of the fluid approaching the contraction. To solve this problem, you must somehow
estimate the flow field near the contraction.

air flow with a repentine area reduction and next atmospheric evacuation

This project simulates compressible turbulent flow through a de Laval nozzle.

compressible flow | SimScale Project Library | Page 1