%0 Generic %A LeBlanc, Bruce %A Vire, Axelle %A Steiner, Julia %A Timmer, Nando %A Langedijk, Emiel %A Bernardy, Stefan %D 2021 %T ABIBA Airfoil and Slat Measurement Data %U https://data.4tu.nl/articles/dataset/ABIBA_Airfoil_and_Slat_Measurement_Data/14170442/1 %R 10.4121/14170442.v1 %K wind tunnel test %K slat element %K vortex generator %K Aerodynamic Blade Improvements and Boosting by Add-ons (ABIBA) %X

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.


%I 4TU.ResearchData