Aeolus ASP is designed for conceptual and preliminary design of aircraft wings. It can also be used for propeller blades. This section shows comparisons of the computational results with wind tunnel data and CFD results.
The report below compares the wing surface pressure distribution and induced drag for 3 wing configurations:
As result, Aeolus ASP shows excellent agreement with wind tunnel measurements.
Aerodynamic simulations on propellers were compared against wind tunnel results and OEM specifications. Thrust, power, and efficiency plots confirm a good agreement between simulations and experiment.
We are constantly looking for new test cases and benchmarks. For questions, remarks, or other validation cases, please do not hesitate to contact us.