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  • 1
    Publication Date: 2019-07-13
    Description: In 2011, the heat exchanger and refrigeration plant for NASA Glenn Research Center's Icing Research Tunnel (IRT) were upgraded. Flow quality surveys were performed in the settling chamber of the IRT in order to understand the effect that the new heat exchanger had on the flow quality upstream of the spray bars. Measurements were made of the total pressure, static pressure, total temperature, airspeed, and ow angle (pitch and yaw). These measurements were directly compared to measurements taken in 2000, after the previous heat exchanger was installed. In general, the flow quality appears to have improved with the new heat exchanger.
    Keywords: Aerodynamics
    Type: E-18455-1 , AIAA 4th Atmospheric Sciences; Jun 25, 2012 - Jun 29, 2012; New Orleans, LA; United States
    Format: application/pdf
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  • 2
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    In:  CASI
    Publication Date: 2019-07-12
    Description: No abstract available
    Keywords: Meteorology and Climatology
    Type: E-661271
    Format: application/pdf
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  • 3
    Publication Date: 2019-08-01
    Description: This presentation is intended for a technical audience. It describes NASA Glenn's two icing-capable facilities, the Icing Research Tunnel (IRT) and the Propulsion Systems Lab (PSL). The presentation contains stock images publicly available from NASA and other sources.
    Keywords: Research and Support Facilities (Air); Air Transportation and Safety
    Type: GRC-E-DAA-TN41480 , University of Notre Dame Dept. of Aerospace and Mechanical Engineering Seminar; Apr 21, 2017; South Bend, IN; United States
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  • 4
    Publication Date: 2019-07-13
    Description: The Icing Research Tunnel at NASA Glenn has recently switched to from using the Icing Blade to using the SEA Multi-Element Sensor (also known as the multi-wire) for its calibration of cloud liquid water content. In order to perform this transition, tests were completed to compare the Multi-Element Sensor to the Icing Blade, particularly with respect to liquid water content, airspeed, and drop size. The two instruments were found to compare well for the majority of Appendix C conditions. However, it was discovered that the Icing Blade under-measures when the conditions approach the Ludlam Limit. This paper also describes data processing procedures for the Multi-Element Sensor in the IRT, including collection efficiency corrections, mounting underneath a splitter plate, and correcting for a jump in the compensation wire power. Further data is presented to describe the repeatability of the IRT with the Multi-Element sensor, health-monitoring checks for the instrument, and a sensing-element configuration comparison.
    Keywords: Research and Support Facilities (Air)
    Type: GRC-E-DAA-TN31930 , Aviation and Aeronautics Forum and Exposition; Jun 13, 2017 - Jun 17, 2017; Washington, DC; United States
    Format: application/pdf
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