Investigation of icing characteristics of typical light-airplane engine induction systems

Willard D. Coles
naca-tn-1790
Feb 1949


The icing characteristics of two typical light-airplane engine induction systems were investigated using the carburators and manifolds of engines in the horsepower ranges from 65 to 85 and 165 to 185.

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http://naca.central.cranfield.ac.uk/reports/1949/naca-tn-1790.pdf