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To find out the drag coefficient of my parachute

Finding terminal velocity and coefficient of drag of the stages of the rocket

Validation of the fastback detailed underbody model

I'm engineer helping my designer friend to learn what is the drag coefficient of his model

- The goal is calculate the drag coefficient
- Incompressible flow

To obtain aerodynamic quantities of interest such as induced drag and drag coefficient of S-10 truck.

Find the drag coefficient of the three-finned model rocket going 155 m/s.

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.

Aerofoil in a different number of angle of attacks then measuring the drag coefficient of that wing.

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