https://doi.org/10.1051/epjconf/201611402026
Properties of Broezel static probe
Technical University of Kosice, Faculty of Aeronautics, Rampova 71, 041 21, Kosice, Slovakia
a Corresponding author: peter.gasparovic@tuke.sk
Published online: 28 March 2016
The properties of flat static probe designed by Broezel and used in sailplanes are investigated for its planned use in low speed tunnel. Both the numerical CFD model and experiment in low speed wind tunnel confirm yaw insensitivity of the static pressure measured by the probe. The results indicate that the probe is sufficiently accurate for its planned use in wind tunnel measurements.
© Owned by the authors, published by EDP Sciences, 2016
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
