A Thermal Analysis of a Hot-Wire Probe for Icing ApplicationsThis paper presents a steady-state thermal model of a hot-wire instrument applicable to atmospheric measurement of water content in clouds. In this application, the power required to maintain the wire at a given temperature is used to deduce the water content of the cloud. The model considers electrical resistive heating, axial conduction, convection to the flow, radiation to the surroundings, as well as energy loss due to the heating, melting, and evaporation of impinging liquid and or ice. All of these parameters can be varied axially along the wire. The model further introduces a parameter called the evaporation potential which locally gauges the maximum fraction of incoming water that evaporates. The primary outputs of the model are the steady-state power required to maintain a spatially-average constant temperature as well as the variation of that temperature and other parameters along the wire. The model is used to understand the sensitivity of the hot-wire performance to various flow and boundary conditions including a detailed comparison of dry air and wet (i.e. cloud-on) conditions. The steady-state power values are compared to experimental results from a Science Engineering Associates (SEA) Multi-Element probe, a commonly used water-content measurement instrument. The model results show good agreement with experiment for both dry and cloud-on conditions with liquid water content. For ice, the experimental measurements under read the actual water content due to incomplete evaporation and splashing. Model results, which account for incomplete evaporation, are still higher than experimental results where the discrepancy is attributed to splashing mass-loss which is not accounted in the model.
Document ID
20150000744
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Struk, Peter M. (NASA Glenn Research Center Cleveland, OH United States)
Rigby, David L. (Vantage Partners, LLC Brook Park, OH, United States)
Venkataraman, Krishna (Texas Univ. Austin, TX, United States)
Date Acquired
January 26, 2015
Publication Date
June 16, 2014
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
GRC-E-DAA-TN15563Report Number: GRC-E-DAA-TN15563
Meeting Information
Meeting: (AVIATION 2014) AIAA Aviation and Aeronautics Forum and Exposition
Location: Atlanta, GA
Country: United States
Start Date: June 16, 2014
End Date: June 20, 2014
Sponsors: American Inst. of Aeronautics and Astronautics