20th Aerospace Sciences Meeting · 1982 · 19 citations · 1 references
EngineeringAerospace EngineeringAerodynamicsAerospace StructuresAircraft StructuresAerodynamic DesignAirfoil TheoryExperimental AerodynamicsIcing ConditionsWing AerodynamicsWing DesignAirfoil AerodynamicsAirfoil DesignExperimental Study DesignIce Accretion EffectsIce Crystal IcingRime IceRime Icing
A full scale general aviation wing with a NACA 63 sub 2 A415 airfoil section was tested to determine icing characteristics for representative rime and glaze icing conditions. Measurements were made of ice accretion shapes and resultant wing section drag coefficient levels. It was found that the NACA 63 sub 2 A415 wing section was less sensitive to rime and glaze icing encounters for climb conditions.
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An analytical approach to airfoil icing
M. B. Bragg, G. M. Gregorek, R.W. Shaw · 19th Aerospace Sciences Meeting · 1981 · 47 citations