Prediction of ice shapes and their effect on airfoil drag

Calculation of ice shapes and the resulting drag increases are presented for a NACA 0012 airfoil. Based on experimental data, an improved correlation of equivalent sand-grain roughness was developed.

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Veröffentlicht in:Journal of aircraft 1994-03, Vol.31 (2), p.263-270
Hauptverfasser: Shin, Jaiwon, Berkowitz, Brian, Chen, Hsun H, Cebeci, Tuncer
Format: Artikel
Sprache:eng
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Zusammenfassung:Calculation of ice shapes and the resulting drag increases are presented for a NACA 0012 airfoil. Based on experimental data, an improved correlation of equivalent sand-grain roughness was developed.
ISSN:0021-8669
1533-3868
DOI:10.2514/3.46483