Three Dimensional Surface Redefinition Method for Computational Ice Accretion SolversComputational tools have been increasing in maturity and are thus commonly used in the engineering design process. Advancements in NASA’s current state of the art computational ice accretion tool are required to tackle the icing challenges of tomorrow. GlennICE, a next generation ice accretion solver, is under development at NASA to tackle these challenges. One of the elements of this migration is transitioning from a quasi-three dimensional strip theory based ice accretion methodology to a fully three dimensional methodology. This requires construction of a method to redefine or extrude a discretized or tessellated surface geometry based on the predicted volumetric ice growth for each tessellated surface triangle. This paper describes the methodology that is employed in the GlennICE software, and assesses the performance of the method in replicating a well defined analytical test case.
Document ID
20205001501
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Christopher Edward Porter (Glenn Research Center Cleveland, Ohio, United States)
David L Rigby (Vantage Partners, LLC NASA Glenn Research Center)
Date Acquired
April 28, 2020
Subject Category
Aeronautics (General)
Meeting Information
Meeting: AIAA Aviation Forum
Location: Reno, NV
Country: US
Start Date: June 15, 2020
End Date: June 19, 2020
Sponsors: American Institute of Aeronautics and Astronautics