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
The High Lift Common Research Model (HL-CRM) is a transonic transport type aircraft consisting of fuselage, wing, single leading-edge slat, and two trailing edge flaps.
This geometry model represents a revision to the original HL-CRM used by HiLiftPW-3. The revision addresses findings from GMGW-1. The modifications are limited to the fuselage and side of body fairing and are detailed in AIAA paper 2018-0130.
For GMGW-1 and/or HiLiftPW-3 participants, note that GMGW-2 Case 1 involves only the full gap configuration (i.e. the gap between the inboard and outboard sections of the flap is fully open and unsealed.)
Download the HL-CRM rev. 2 geometry model from the workshop ftp site.
Right click on the file link and use Save link as.