Design, construction and commissioning of the Braunschweig Icing Wind Tunnel
-
Published:2018-06-06
Issue:6
Volume:11
Page:3221-3249
-
ISSN:1867-8548
-
Container-title:Atmospheric Measurement Techniques
-
language:en
-
Short-container-title:Atmos. Meas. Tech.
Author:
Bansmer Stephan E., Baumert Arne, Sattler Stephan, Knop Inken, Leroy Delphine, Schwarzenboeck Alfons, Jurkat-Witschas Tina, Voigt ChristianeORCID, Pervier Hugo, Esposito Biagio
Abstract
Abstract. Beyond its physical importance in both fundamental and
climate research, atmospheric icing is considered as a severe operational
condition in many engineering applications like aviation, electrical power
transmission and wind-energy production. To reproduce such icing conditions
in a laboratory environment, icing wind tunnels are frequently used. In this
paper, a comprehensive overview on the design, construction and commissioning
of the Braunschweig Icing Wind Tunnel is given. The tunnel features a test
section of 0.5 m × 0.5 m with peak velocities of up to
40 m s−1. The static air temperature ranges from −25 to
+30 ∘C. Supercooled droplet icing with liquid water contents up to
3 g m−3 can be reproduced. The unique aspect of this facility is
the combination of an icing tunnel with a cloud chamber system for making ice
particles. These ice particles are more realistic in shape and density than
those usually used for mixed phase and ice crystal icing experiments. Ice water contents up to 20 g m−3 can be generated. We further show
how current state-of-the-art measurement techniques for particle sizing are
performed on ice particles. The data are compared to those of in-flight
measurements in mesoscale convective cloud systems in tropical regions.
Finally, some applications of the icing wind tunnel are presented.
Funder
Deutsche Forschungsgemeinschaft Bundesministerium für Wirtschaft und Energie Seventh Framework Programme Helmholtz-Gemeinschaft
Publisher
Copernicus GmbH
Subject
Atmospheric Science
Reference66 articles.
1. Al-Khalil, K., Salamon, L., and Tenison, G.: Development of the Cox icing
research facility, in: 36th Aerospace Sciences Meeting & Exhibit, AIAA,
Citeseer, 1998. a 2. Bansmer, S. E. and Baumert, A.: From high altitude clouds to an icing wind
tunnel: en route to understand ice crystal icing, in: Proceedings of the
EUCASS Conference held in Milano, Italy, 2017. a 3. Baumert, A., Bansmer, S., Sattler, S., Pervier, H., and Esposito, B.:
Simulating natural ice crystal cloud conditions for icing wind tunnel
experiments – A review on the design, commissioning and calibration of the TU
Braunschweig ice crystal generation system, in: AIAA AVIATION Forum,
American Institute of Aeronautics and Astronautics,
https://doi.org/10.2514/6.2016-4053, 2016. a, b 4. Baumert, A., Bansmer, S., Trontin, P., and Villedieu, P.: Experimental and
numerical investigations on aircraft icing at mixed phase conditions,
Int. J. Heat Mass Tran., 123, 957–978, 2018. a 5. Beaugendre, H., Morency, F., and Habashi, W. G.: FENSAP-ICE's Three-Dimensional
In-Flight Ice Accretion Module: ICE3D, J. Aircraft, 40, 239–247,
https://doi.org/10.2514/2.3113, 2003. a
Cited by
52 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
|
|