Report presents results of wind-tunnel tests of aerodynamic effects of deicing and anti-icing fluids on airplane wings. Tests conducted on three-dimensional half-model airplane and two-dimensional airfoil model at temperatures ranging from -29 to +10 degrees C. Fluids used included three commercial fluids available for use during 1987-1988 winter season, one discontinued commercial fluid, and eight newer fluids experimental at time of test.
Aerodynamic Effects Of Deicing And Anti-Icing Fluids
NASA Tech Briefs ; 18 , 2
1994-02-01
Miscellaneous
No indication
English
Aerodynamic Effects of Deicing and Anti-Icing Fluids
Online Contents | 1994
Aerodynamic Effects of Deicing and Anti-Icing Fluids
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