H2020 ENODISE: TUD Experimental database configuration B1

H2020 ENODISE project data contains experimental measurements for aerodynamics and acoustics of configuration B1. The data was collected in the Low-Speed, Low-Turbulence Tunnel at Delft University of Technology using a Distributed Electric Propulsion wing model with three propellers. Author Fernanda d. Monteiro from Delft University of Technology contributed this dataset.

Use Cases

• Validate computational fluid dynamics (CFD) models based on aerodynamic wind tunnel data.
• Analyze noise profiles and acoustic signatures based on the described propeller configuration.
• Study aerodynamic interference effects based on the side-by-side propeller installation on a wing.

Strengths

• Data originates from a controlled experimental setup in a university wind tunnel.
• Focuses on a specific, modern aircraft propulsion configuration (Distributed Electric Propulsion).
• Dataset is associated with a defined European research project (H2020 ENODISE).

Limitations

• Column-level documentation is absent; field semantics must be inferred after download.
• Row count is unknown, which may limit suitability assessment.
• Last update date is unknown; freshness unverified.

Provenance

Source

Delft University of Technology

Collection Method

Experimental measurements in the Low-Speed, Low-Turbulence Tunnel (LTT).