ABIBA Airfoil and Slat Measurement Data

doi: 10.4121/14170442.v2
The doi above is for this specific version of this dataset, which is currently the latest. Newer versions may be published in the future. For a link that will always point to the latest version, please use
doi: 10.4121/14170442
Datacite citation style:
LeBlanc, Bruce; Vire, Axelle; Steiner, Julia; Timmer, Nando; Langedijk, Emiel et. al. (2021): ABIBA Airfoil and Slat Measurement Data. Version 2. 4TU.ResearchData. dataset. https://doi.org/10.4121/14170442.v2
Other citation styles (APA, Harvard, MLA, Vancouver, Chicago, IEEE) available at Datacite
choose version:
version 2 - 2021-03-15 (latest)
version 1 - 2021-03-09

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.

  • 2021-03-09 first online
  • 2021-03-15 published, posted
  • 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)


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