Univ. of British Columbia
NASA Langley Research Center
National Aerospace Solutions
The Boeing Company
MBDA UK Ltd
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.