John Chawner
Pointwise, Inc.
John Dannenhoffer
Syracuse University
Mark Gammon
ITI
Carl Ollivier-Gooch
Univ. of British Columbia
Bill Jones
NASA Langley Research Center
James Masters
National Aerospace Solutions
Todd Michal
The Boeing Company
Nigel Taylor
MBDA UK Ltd
Hugh Thornburg
Engility
Carolyn Woeber
Pointwise, Inc.
meshingworkshop@gmail.com
A wind tunnel model of the NASA High-Lift Common Research Model (HL-CRM) has been designed to provide experimental data for 4th AIAA High-Lift Prediction Workshop. This presentation will review the salient aspects of the geometry model used to define this wind tunnel test hardware from the viewpoint of its use for mesh generation and CFD. Building on the material provided in previous presentations on the NASA CRM and HL-CRM geometry models that were designed specifically for numerical simulation, this presentation will focus on identifying any additional aspects that may have been introduced as a consequence of the requirements to have the model manufactured.