Original title: Small Icing Wind Tunnel
Authors: Horák, V. ; Hoření, Bohumír ; Rozehnal, D. ; Svoboda, E.
Document type: Papers
Conference/Event: ICMT'07, The international conference on military technologies, Brno (CZ), 2007-05-02 / 2007-05-04
Year: 2007
Language: eng
Abstract: The paper deals with a small icing wind tunnel realized at the Department of Aerospace and Rocket Technologies in conjunction with the aircraft icing simulation project. There are presented some results of the airfoil ice accretion prediction and various resulting ice shapes from icing wind tunnel. Appropriate consideration is given to the ice shape geometry measurement either.
Keywords: aircraft icing; ice accretion; icing wind tunnel
Project no.: CEZ:AV0Z20600510 (CEP), FT-TA/026 (CEP)
Funding provider: GA MPO
Host item entry: Proceedings of the International Conference on Military Technologies 2007 (ICMT'07), ISBN 978-80-7231-238-2

Institution: Institute of Hydrodynamics AS ČR (web)
Document availability information: Fulltext is available at the institute of the Academy of Sciences.
Original record: http://hdl.handle.net/11104/0196960

Permalink: http://www.nusl.cz/ntk/nusl-42764


The record appears in these collections:
Research > Institutes ASCR > Institute of Hydrodynamics
Conference materials > Papers