Abstract
A multi-step version of the aircraft icing code ICECREMO2 is used to simulate ice layers in cold and mild conditions. The models used are presented and results are compared with available data. The modifications necessary to introduce anti- or de-icing devices in the model are also discussed.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
Gent, R.W., Dart, N.P., Cansdale, J.T.: Phil. Trans. R. Soc. Lond. A 358, 2873–2911 (2000)
Harireche, O., Verdin, P., Thompson, C.P., Hammond, D.W.: J. Aircr. 45(6), 1924–1936 (2008)
Kind, R.J.: NATO-RTO, TR-038 (2001)
Kind, R.J., Potapczuk, M.G., Feo, A., Golia, C., Shah, A.D.: Prog. Aerosp. Sci. 34, 257–345 (1998)
Myers, T.G., Charpin, J.P.F.: Int. J. Heat Mass Transf. 47, 5483–5500 (2004)
Myers, T.G., Charpin, J.P.F., Chapman, S.J.: Phys. Fluids 14, 2788–2803 (2002)
Shin, J., Bond, T.H.: AIAA 92-0647 (1992)
Verdin, P., Charpin, J.P.F., Thompson, C.P.: J. Aircr. 46(5), 1607–1613 (2009)
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2010 Springer-Verlag Berlin Heidelberg
About this chapter
Cite this chapter
Charpin, J.P.F., Verdin, P. (2010). Multi-Stepping and Anti-Icing / De-Icing Devices. In: Fitt, A., Norbury, J., Ockendon, H., Wilson, E. (eds) Progress in Industrial Mathematics at ECMI 2008. Mathematics in Industry(), vol 15. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-12110-4_35
Download citation
DOI: https://doi.org/10.1007/978-3-642-12110-4_35
Published:
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-12109-8
Online ISBN: 978-3-642-12110-4
eBook Packages: Mathematics and StatisticsMathematics and Statistics (R0)