Total Temperature Measurements in Icing Cloud Flows Using a Rearward Facing Probe

Agui, Juan H ; Struk, Peter M ; Bartkus, Tadas P

关键词: AIR FLOW;    ATMOSPHERIC TEMPERATURE;    COMPUTATIONAL FLUID DYNAMICS;    DYNAMIC MODELS;    ELECTROMAGNETIC ABSORPTION;    FLOW CHARACTERISTICS;    HIGH TEMPERATURE ENVIRONMENTS;    HUMIDITY MEASUREMENT;    ICE FORMATION;    METEOROLOGY;    PARTICLE SIZE DISTRIBUTION;    PROPULSION SYSTEM CONFIGURATIONS;    PROPULSION SYSTEM PERFORMANCE;    TEMPERATURE PROBES;    THERMODYNAMICS;   

RP-ID  :  GRC-E-DAA-TN67171

学科分类：工程和技术（综合）

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

This paper reports on temperature and humidity measurements from a series of ice-crystal icing tunnel experiments conducted in June 2018 at the Propulsion Systems Laboratory at the NASA Glenn Research Center. The tests were fundamental in nature and were aimed at investigating the icing processes on a two-dimensional NACA0012 airfoil subjected to artificially generated icing clouds. Prior to the tests on the airfoil, a suite of instruments, including total temperature and humidity probes, were used to characterize the thermodynamic flow and icing cloud conditions of the facility. Two different total temperature probes were used in these tests which included a custom designed rearward facing probe and a commercial self-heating total temperature probe. The rearward facing probe, the main total temperature probe, was designed to reduce and mitigate the contaminating effects of icing and ingestion of ice crystals and water droplets at the probe's inlet. The probe also serves as an air-sample inlet for a light absorption based humidity measurement. The paper includes a section which discusses total temperature and humidity measurement considerations, and another section which provides an analysis of the main probe's performance characteristics. A computational fluid dynamic model of the flow around the probe was also conducted to gain insight into the trajectory of the flow entering the probe inlet. The experiments included a series of tests in which the relative humidity of the facility flow was swept through with increasingly larger values. The data showed that the rearward facing probe can reasonably capture the flow's total temperature and humidity under mild to moderate icing conditions but produces anomalous results under more intense icing conditions. The experimental data was also compared to an in-house developed thermodynamic model which takes into account the interaction of the main flow with the icing cloud. Comparison to the thermodynamic model showed that the rearward facing probe measured the predicted trends.