TECHNICAL PAPERS

Experimental Study of the Scallop Formation on Swept Cylinder

Date Published: 2007-09-24
Paper Number: 2007-01-3296
DOI: 10.4271/2007-01-3296

Citation:

Presteau, X., Montreuil, E., Leroy, A., Guffond, D. et al., "Experimental Study of the Scallop Formation on Swept Cylinder," SAE Technical Paper 2007-01-3296, 2007, doi:10.4271/2007-01-3296.

Author(s):


Xuan Presteau - DMPH, Onera
Emmanuel Montreuil - DMPH, Onera
Alexandre Leroy - DMPH, Onera
Didier Guffond - DMPH, Onera
Robert Henry - DMPH, Onera
Pascal Personne - LaMP, Blaise PASCAL Univ.

Abstract:

Two-dimensional models have been developed to predict and reproduce ice accretion shapes on airfoil profiles. These simulated shapes mostly are similar to experimental forms. However, in some conditions, the ice shapes could present some discontinuity along span showing some ice deposit separated by air inclusion: this deposit is called “lobster tail” or “scallop icing”. The classical 2D approaches fail to predict this kind of ice shapes. The 3D simulation requires to take into account a fully detailed heat and mass balance parameters which scallop accretion is sensitive. For that, the scallop formation was experimentally led on the swept cylinders.

File Size: 6747K

Product Status: In Stock

See papers presented at 2007 SAE Aircraft and Engine Icing International Conference, September 2007, Seville, SPAIN, Session: Icing Physics

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