A Trajectory Refinement Scheme for Arbitrary Triangularly Tessellated BoundariesGlennICE relies on a Delaunay triangulation step to generate a two dimensional mesh of the point cloud of trajectory release locations in its adaptive refinement process. Previously GlennICE performed a 2.5D Delaunay triangulation to generate a two dimensional mesh from a point cloud in three-dimensional space. This process is not a general scheme and contains restrictions that prohibit GlennICE from being extended to tackle new challenges. This paper introduces a new method that does not rely on a 2.5D Delaunay triangulation, and instead performs a triangulation directly on the tessellated inlet surface. It accomplishes this by performing a triangulation on the local point cloud associated with each triangular face of the tessellated inlet surface. Each of these local triangulations are stitched together to form a single contiguous mesh. While the resulting mesh is not guaranteed to be a valid Delaunay triangulation, this formulation is significantly more general than its predecessor and enables the GlennICE code to be extended for a variety of different applications. This includes the ability to extend the software to handle reentraining splashed, bounced, or broken droplets and crystals.
Document ID
20250005546
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Christopher E. Porter (Glenn Research Center Cleveland, United States)
Eric T. Galloway (HX5 (United States) Fort Walton Beach, Florida, United States)
David L. Rigby (HX5 (United States) Fort Walton Beach, Florida, United States)
William B. Wright (HX5 (United States) Fort Walton Beach, Florida, United States)
Date Acquired
May 28, 2025
Subject Category
Aircraft Design, Testing and Performance
Meeting Information
Meeting: AIAA Aviation Forum
Location: Las Vegas, NV
Country: US
Start Date: July 21, 2025
End Date: July 25, 2025
Sponsors: American Institute of Aeronautics and Astronautics