This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Effect of Icing Environment and Humidity on Reference Air Data Parameters in an Icing Tunnel
Technical Paper
2019-01-1929
ISSN: 0148-7191, e-ISSN: 2688-3627
Annotation ability available
Sector:
Language:
English
Abstract
Wind tunnel facilities typically rely upon reference instrumentation combined with isentropic flow relationships to define the fluid properties in the test section. For the particular case of icing wind tunnels, the icing environment can affect the airflow such that the definition of test section parameters via isentropic relationships is not strictly correct. These influences are of particular importance for testing air data probes because the nature of the test is to evaluate the performance of a sensor directly measuring the parameters being affected. Momentum, heat, and mass transfer from the water phase to the air phase can result in total temperature and total pressure measurements in the test section that differ from those measured at an upstream station, where reference measurements are typically taken. This effect was first observed by Luers & Fiscus [1] in the context of wind tunnel tests for heavy rain conditions.
Recommended Content
| Journal Article | Four Years of Testing to AS5562 |
| Journal Article | Development of a Coupled Air and Particle Thermal Model for Engine Icing Test Facilities |
| Technical Paper | Total Temperature Measurements in Icing Cloud Flows Using a Rearward Facing Probe |
Authors
Citation
Whalen, M. and Matheis, B., "Effect of Icing Environment and Humidity on Reference Air Data Parameters in an Icing Tunnel," SAE Technical Paper 2019-01-1929, 2019, https://doi.org/10.4271/2019-01-1929.Also In
References
- Luers , J. and Fiscus , I. Performance of an A-Vane and Pitot Tube in Simulated Heavy Rain Environment University of Dayton Research Institute 1985
- Bartkus , T. et.al. Comparisons of Mixed-Phase Icing Cloud Simulations with Experiments Conducted at the NASA Propulsion Systems Laboratory 9th AIAA Atmospheric and Space Environments Conference 2017
- Agui , J. et.al. Total Temperature Measurements Using a Rearward Facing Probe in Supercooled Liquid Droplet and Ice Crystal Clouds AIAA Atmospheric and Space Environments Conference 2018
- SAE International Aerospace Standard Ice and Rain Minimum Qualification Standards for Pitot and Pitot-static Probes SAE Standard AS5562 2015