MATEC Web Conf.
Volume 168, 2018XXI. International Scientific Conference - The Application of Experimental and Numerical Methods in Fluid Mechanics and Energy 2018 (AEaNMiFMaE-2018)
|Number of page(s)||10|
|Section||Special Experimental Methods in Fluid Mechanics and Energy|
|Published online||23 May 2018|
Experimental investigation of the boundary layer transition on the prismatic blade using infrared thermography
VZLU - Czech Aerospace Research Centre, Beranových 130, 199 05 Prague, Czech Republic
* Corresponding author: email@example.com
Topic of this contribution is the detection of the laminar-turbulent boundary layer transition on the prismatic blade using infrared thermography. Several Reynolds and Mach numbers were investigated, and their influence on the boundary layer transition was evaluated. Results are in good agreement with experiments that were performed earlier with hot-film anemometry.
© The Authors, published by EDP Sciences, 2018
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. (http://creativecommons.org/licenses/by/4.0/).
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