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

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

Dataset

x choose version: version 1 - 2021-03-09

• Aerospace Engineering

Aerodynamic Blade Improvements and Boosting by Add-ons (ABIBA), slat element, vortex generator, wind tunnel test

CC0

RefWorks, BibTeX, Reference Manager, Endnote, DataCite, NLM, DC, CFF

by Bruce LeBlanc , Axelle 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.

• 2021-03-09 first online

• 2021-03-15 published, posted

4TU.ResearchData

• 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)