Empirical equation developed by which changes in drag coefficients due to ice formations on NACA 65A004 airfoil may be calculated from known icing and flight conditions; extended equation includes data for other airfoils up to 15% thickness ratio; estimation of lift and pitching moment coefficients.
Correlation of airfoil ice formations and their aerodynamic effects with impingement and flight conditions
Soc Automotive Engrs -- Paper
Society of Automotive Engineers -- Meeting ; 1957 Ice problems
1957
10 pages
Conference paper
English
© Metadata Copyright Elsevier B. V. All rights reserved.
SAE Technical Papers | 1957
|OPERATIONALIZING FLIGHT FORMATIONS FOR AERODYNAMIC BENEFITS
TIBKAT | 2020
|Cascade Impingement Cooled Airfoil
NTIS | 2004
|