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In-flight Ice formation simulation on finite wings and air intakes

Published online by Cambridge University Press:  27 January 2016

S. Özgen  and
M. Canıbek
S. Özgen*
Affiliation:
Middle East Technical University, Dept. Aerospace Engineering, Ankara, Turkey
M. Canıbek*
Affiliation:
Turkish Aerospace Industries, Flight Sciences Department, Ankara, Turkey
*
[email protected]
[email protected]
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Abstract

In the present article, in-flight ice formation on finite wings and air intakes of low-speed aircraft are numerically studied. The approach to the problem involves calculation of the velocity field using a three-dimensional panel method. Using the calculated velocity field, the droplet trajectories and droplet impact locations are computed yielding the droplet collection efficiency distribution. In the next step, convective heat transfer coefficient distributions around the geometries are calculated using a two-dimensional Integral Boundary-Layer Method, which takes surface roughness due to ice accretion into account. A thermodynamic analysis employing the Extended Messinger Method yields the ice growth rates. Integration of these rates over time yields the ice shapes, hence the modified geometry. Predicted ice shapes are compared with experimental shapes reported in the literature and good agreement is observed. Ice shapes around vastly varying geometries including complex shapes are successfully computed. As such, the developed tool may be used for academical purposes or for airworthiness certification efforts.

Type
Research Article
Information
The Aeronautical Journal , Volume 116 , Issue 1178 , April 2012 , pp. 337 - 362
Copyright
Copyright © Royal Aeronautical Society 2012 

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References

1. Özgen, S. and Canibek, M. Ice accretion simulation on multi-element aerofoils using extended Messinger model, Heat and Mass Transfer, 2009, 45, (3), pp 305–322.Google Scholar
2. Myers, T.G. Extension to the messinger model for aircraft icing, AIAA J, 2001, 39, pp 211–218.Google Scholar
3. Potapczuk, M.G. and Bidwell, C.S. Swept wing ice accretion modeling, NASA TM-103114, 1990.Google Scholar
4. Mingione, G., Brandi, V. and Saporiti, A. A 3D Ice accretion simulation code, AIAA Paper 99-0247, 1999.Google Scholar
5. Cebeci, T. and Besnard, E. Prediction of the performance degradation of aircraft in natural icing conditions, AIAA Paper 94-0487, 1994.Google Scholar
6. Papadakis, M., Wong, S.-C., Rachman, A., Hung, K.E., Vu, G.T. and Bidwell, C.S. Large and small droplet impingement data on aerofoils and two simulated ice shapes, NASA TM-2007-213959, 2007.Google Scholar
7. KatZ, J. and Plotkin, A. Low-Speed Aerodynamics, 2nd ed, Cambridge University Press, Cambridge, UK, 2001.Google Scholar
8. Paraschiviou, I. and Saeed, F. Aircraft Icing, 2007 (unpublished book draft).Google Scholar
9. Caruso, S.C. NEARICE: An Unstructed-Mesh Navier-Stokes-Based Ice Accretion Prediction Method, AIAA Paper 94-0606, 1994.Google Scholar
10. Jeck, R.K. Meteorological data for use in simulation icing conditions in Ice Accretion Simulation, AGARD-AR-344, 1997.Google Scholar
11. Clift, R., Grace, J.R. and Weber, M.E. Bubbles, Drops and Particles, Academic Press, New York, USA, 1978.Google Scholar
12. Schlichting, H. Boundary Layer Theory, 7th ed, McGraw-Hill, New York, USA, 1979.Google Scholar
13. Wright, W.B., Gent, R.W. and Guffond, D. DRA/NASA/ONERA collaboration on icing research, part II- prediction of aerofoil ice accretion, NASA CR-202349, 1997.Google Scholar
14. Gent, R.W., Dart, N.P. and Cansdale, J.T. Aircraft icing, Phil Trans R Soc Lond A, 2000, 358, pp 2873–2911.Google Scholar
15. Myers, T.G., Charpin, J.P.F. and Thompson, C.P. Slowly accreting ice due to supercooled water impacting on a cold surface, Phys Fluids, 2002, 14, (1), pp 240–256.Google Scholar
16. Fortin, G., Laforte, J.-L. and Ilinca, A. Heat and mass transfer during ice accretion on aircraft wings with an improved roughness model, Int J Thermal Sciences, 2006, 45, pp 595–606.Google Scholar