TY - DATA T1 - ABIBA Airfoil and Slat Measurement Data PY - 2021/03/15 AU - Bruce LeBlanc AU - Axelle Vire AU - Julia Steiner AU - Nando Timmer AU - Emiel Langedijk AU - Stefan Bernardy UR - https://data.4tu.nl/articles/dataset/ABIBA_Airfoil_and_Slat_Measurement_Data/14170442/2 DO - 10.4121/14170442.v2 KW - wind tunnel test KW - slat element KW - vortex generator KW - Aerodynamic Blade Improvements and Boosting by Add-ons (ABIBA) N2 -

Dataset for the ABIBA experiments. The data was collected at the Delft University of Technology's Low Turbulence Tunnel in summer of 2020.

Data includes:

· Report summarizing results

· Geometry and pressure tap locations for the base airfoil (DU-00 W2-401)

· Geometry and pressure tap locations for custom slat profile

· Final experimental polars

· Cp data for slat and profile for each testing configuration

Pictures of measurement setup

Measurement is conducted at a Re: 1.5 x 106 and 2.0 x 106

The base airfoil is measured in three configurations; clean, tripped, and with vortex generators. There are 9 different slat configurations as discussed in the included report. Each are measured in clean and tripped conditions.


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