Aircraft icing

Author:

Gent R. W.1,Dart N. P.1,Cansdale J. T.1

Affiliation:

1. Defence Evaluation and Research Agency, Farnborough, Hampshire GU14 0LX, UK

Publisher

The Royal Society

Subject

General Physics and Astronomy,General Engineering,General Mathematics

Reference56 articles.

1. The e® ect of surface roughness on the heat transfer from a circular cylinder to the cross ow of air;Achenbach E.;Inst. J. Heat Mass Transfer,1977

2. AGARD 1997 (Advisory Group for Aerospace Research & Development) Ice accretion simulation. Report of Fluid Dynamics Panel Working Group 20. NATO report AGARD-AR-344 December 1997.

3. Allan M. R. 1998 Application of PMB2D unsteady Navier{Stokes solver for estimation of iced aerofoil performance. DERA/MSS/CR980544 October 1998.

4. Ashill P. R. Woods R. F. & Weeks D. J. 1987 An improved semi-inverse version of the Viscous Garabedian and Korn method (VGK). RAE TR87002 January 1987.

5. Bartlett P. 2000 Development of a new model of ice accretion on aircraft. In 9th Int. Workshop on Atmospheric Icing of Structures (IWAIS 2000) 5{8 June Chester UK.

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