Ice Accretion Measurements on an Airfoil and Wedge in Mixed-Phase ConditionsThis paper describes ice accretion measurements from experiments conducted at the National Research Council (NRC) of Canada's Research Altitude Test Facility during 2012. Due to numerous engine power loss events associated with high altitude convective weather, potential ice accretion within an engine due to ice crystal ingestion is being investigated collaboratively by NASA and NRC. These investigations examine the physical mechanisms of ice accretion on surfaces exposed to ice crystal and mixed phase conditions, similar to those believed to exist in core compressor regions of jet engines. A further objective of these tests is to examine scaling effects since altitude appears to play a key role in this icing process.
Document ID
20150019658
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Struk, Peter (NASA Glenn Research Center Cleveland, OH United States)
Bartkus, Tadas (Ohio Aerospace Inst. Cleveland, OH, United States)
Tsao, Jen-Ching (Ohio Aerospace Inst. Cleveland, OH, United States)
Currie, Tom (National Research Council of Canada Ottawa, Ontario, Canada)
Fuleki, Dan (National Research Council of Canada Ottawa, Ontario, Canada)
Date Acquired
October 23, 2015
Publication Date
June 22, 2015
Subject Category
Air Transportation And Safety
Report/Patent Number
GRC-E-DAA-TN23445Report Number: GRC-E-DAA-TN23445
Meeting Information
Meeting: 2015 SAE International Conference on Icing of Aircraft, Engines, and Structures