Effect of Pneumatic De-icers and Ice Formations on Aerodynamic Characteristics of an Airfoil

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  • Effect of Pneumatic De-icers and Ice Formations on Aerodynamic Characteristics of an Airfoil Book Detail

  • Author : Dean T. Bowden
  • Release Date : 1956
  • Publisher :
  • Genre : Aerofoils
  • Pages : 710
  • ISBN 13 :
  • File Size : 19,19 MB

Effect of Pneumatic De-icers and Ice Formations on Aerodynamic Characteristics of an Airfoil by Dean T. Bowden PDF Summary

Book Description: Measurements of lift, drag, and pitching moment of an NACA 0011 airfoil were made in icing using two types of pneumatic de-icers, one having spanwise inflatable tubes and the other having chordwise tubes. Ice remaining after inflation of the spanwise-tube de-icer increased airfoil section drag 7 to 37 percent for 0 to 4.6 degrees angle of attack over the ranges of airspeed, total air temperature, liquid-water content, and cycle times covered. This drag increase became constant after a few de-icing cycles. Drag increases due to ice remaining on the chordwise-tube de-icer were similar to those for the spanwise-tube de-icer. Minimum airfoil drag in icing (averaged over a de-icing cycle) was usually obtained with a short (about i min) de-icing cycle.

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NACA Wartime Reports. Series L.

NACA Wartime Reports. Series L.

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In connection with the general study of icing problems an item of major interest is the effect of ice on the aerodynamic characteristics of a wing. Of particula