The Influence of SLD Drop Size Distributions on Ice Accretion in the NASA Icing Research Tunnel
The Influence of SLD Drop Size Distributions on Ice Accretion in the NASA Icing Research Tunnel
Further Examinations of Bimodal SLD Ice Accretion in the NASA Icing Research Tunnel (AIAA 2018-3182)
Development of a Coupled Air and Particle Thermal Model for Engine Icing Test Facilities
Parametric Study of Ice Accretion Formation on a Swept Wing at SLD Conditions
Development of a Coupled Air and Particle Thermal Model for Engine Icing Test Facilities
Ice Accretion Measurements on an Airfoil and Wedge in Mixed-Phase Conditions