9 files

ABIBA Airfoil and Slat Measurement Data

posted on 15.03.2021, 14:38 by Bruce LeBlancBruce LeBlanc, Axelle VireAxelle Vire, Julia Steiner, Nando Timmer, Emiel Langedijk, Stefan Bernardy

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.


Rijksdienst voor Ondernemend Nederland (RVO) through the TSE Hernieuwbare Energie funding scheme (ABIBA project)





TU Delft, Faculty of Aerospace Engineering, Department of Aerodynamics, Wind Energy, Flight Performance & Propulsion (AWEP)