<?xml-stylesheet type="text/xsl" href="https://community.cadence.com/cfs-file/__key/system/syndication/rss.xsl" media="screen"?><rss version="2.0" xmlns:dc="http://purl.org/dc/elements/1.1/" xmlns:slash="http://purl.org/rss/1.0/modules/slash/" xmlns:wfw="http://wellformedweb.org/CommentAPI/"><channel><title>Resolving Boundary Layers with Unstructured Quad and Hex Meshing: On-Demand Webinar</title><link>/cadence_blogs_8/b/cfd/posts/resolving-boundary-layers-with-unstructured-quad-and-hex-meshing-on-demand-webinar-1411081785</link><description>All things being equal, CFD practitioners prefer to use hexahedral mesh cells in the boundary layer for the improved robustness and accuracy they bring to the flow solver. Traditionally, a hex grid would be created using a structured grid technique (</description><dc:language>en-US</dc:language><generator>Telligent Community 12</generator></channel></rss>