Comparisons of Mixed-Phase Icing Cloud Simulations with Experiments Conducted at the NASA Propulsion Systems LaboratoryThis paper builds on previous work that compares numerical simulations of mixed-phase icing clouds with experimental data. The model couples the thermal interaction between ice particles and water droplets of the icing cloud with the flowing air of an icing wind tunnel for simulation of NASA Glenn Research Centers (GRC) Propulsion Systems Laboratory (PSL). Measurements were taken during the Fundamentals of Ice Crystal Icing Physics Tests at the PSL tunnel in March 2016. The tests simulated ice-crystal and mixed-phase icing that relate to ice accretions within turbofan engines.
Document ID
20170007269
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Bartkus, Tadas (Ohio Aerospace Inst. Cleveland, OH, United States)
Tsao, Jen-Ching (Ohio Aerospace Inst. Cleveland, OH, United States)
Struk, Peter (NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
August 3, 2017
Publication Date
June 5, 2017
Subject Category
Aircraft Propulsion And PowerResearch And Support Facilities (Air)
Report/Patent Number
GRC-E-DAA-TN42937Report Number: GRC-E-DAA-TN42937
Meeting Information
Meeting: AIAA Aviation Conference
Location: Denver, CO
Country: United States
Start Date: June 5, 2017
End Date: June 9, 2017
Sponsors: American Inst. of Aeronautics and Astronautics
IDRelationTitle20170007927See AlsoComparisons of Mixed-Phase Icing Cloud Simulations with Experiments Conducted at the NASA Propulsion Systems Laboratory