TY - DATA
T1 - ABIBA Airfoil and Slat Measurement Data
PY - 2021/03/09
AU - Bruce LeBlanc
AU - Axelle Vire
AU - Julia Steiner
AU - Nando Timmer
AU - Emiel Langedijk
AU - Stefan Bernardy
UR - https://data.4tu.nl/articles/dataset/ABIBA_Airfoil_and_Slat_Measurement_Data/14170442/1
DO - 10.4121/14170442.v1
KW - wind tunnel test
KW - slat element
KW - vortex generator
KW - Aerodynamic Blade Improvements and Boosting by Add-ons (ABIBA)
N2 - <p>Dataset for the ABIBA experiments. The data was
collected at the Delft University of Technology's Low Turbulence Tunnel in
summer of 2020.<br>
<br>
Data includes:</p>

<p>·        
Report summarizing results</p>

<p>·        
Geometry and pressure
tap locations for the base airfoil (DU-00 W2-401)</p>

<p>·        
Geometry and pressure
tap locations for custom slat profile</p>

<p>·        
Final experimental polars</p>

<p>·        
Cp data for slat and
profile for each testing configuration</p>

<p> Pictures of measurement setup</p>

<p>Measurement is conducted at a Re: 1.5 x 10<sup>6</sup>
and 2.0 x 10<sup>6</sup></p>

<p> </p>

<p>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.</p>

<p> </p>

<p><br></p>
ER -