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Effects of Ice Formations on Airplane Performance in Level Cruising FlightA flight investigation in natural icing conditions was conducted by the NACA to determine the effect of ice accretion on airplane performance. The maximum loss in propeller efficiency encountered due to ice formation on the propeller blades was 19 percent. During 87 percent of the propeller icing encounters, losses of 10 percent or less were observed. Ice formations on all of the components of the airplane except the propellers during one icing encounter resulted in an increase in parasite drag of the airplane of 81 percent. The control response of the airplane in this condition was marginal.
Document ID
19810068605
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Technical Note
Authors
Preston, G. Merritt
(National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Blackman, Calvin C.
(National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Date Acquired
August 11, 2013
Publication Date
May 1, 1948
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA-TN-1598
Report Number: NACA-TN-1598
Accession Number
81N73027
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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