31st Aerospace Sciences Meeting 1993
DOI: 10.2514/6.1993-301
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An overview of shed ice impact studies in the NASA Lewis Icing Research Tunnel

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Cited by 3 publications
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“…In flight, the ice forms when the temperature is at or slightly below the freezing point and the atmosphere contains supercooled water droplets. Upon hitting the aircraft, these droplets may begin to freeze immediately or flow as a thin film of water on the surface and then freeze [24][25][26]. It is well known that water and ice have distinct dielectric properties and losses, and one can make use of this distinction to sense the onset of ice formation on structures using IDTs.…”
Section: Ice Sensing On Aircraftmentioning
confidence: 99%
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“…In flight, the ice forms when the temperature is at or slightly below the freezing point and the atmosphere contains supercooled water droplets. Upon hitting the aircraft, these droplets may begin to freeze immediately or flow as a thin film of water on the surface and then freeze [24][25][26]. It is well known that water and ice have distinct dielectric properties and losses, and one can make use of this distinction to sense the onset of ice formation on structures using IDTs.…”
Section: Ice Sensing On Aircraftmentioning
confidence: 99%
“…Simulations and experiments on the droplet trajectory and the size distribution on aircraft have been carried out by many authors; see for example [24][25][26]. Following [24], the mass flow rate of water droplets on aircraft surfaces is given by where V inf is the free-stream velocity, S F is the surface area of the wing or blade normal to the free-stream direction, and LWC is the liquid-water content.…”
Section: Ice Sensing On Aircraftmentioning
confidence: 99%