LeBlanc, Bruce; Vire, Axelle; Steiner, Julia; Timmer, Nando; Langedijk, Emiel et. al. (2021): ABIBA Airfoil and Slat Measurement Data. Version 1. 4TU.ResearchData. dataset. https://doi.org/10.4121/14170442.v1

Dataset

x choose version: version 2 - 2021-03-15 (latest)

• 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, 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)