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Fluid flow test of my Mini liquid fuelled rocket engine design.

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

temperatura en camara de combustion del merlin 1 vacio + refrigeracion con O2 liquido

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

Simulation of the aerodinamics of a model rocket

Design and Analysis of Spur Gear for Dynamic Applications

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.

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

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.

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

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

aerospace engineering | SimScale Project Library | Page 1