2nd AIAA Geometry and Mesh Generation Workshop
Sponsored by the Meshing, Visualization, and Computational Environments Technical Committee

January 5-6, 2019
at the AIAA SciTech Forum and Exposition
San Diego, California, USA

GMGW-2
Organizing Committee


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

High Lift Common Research Model

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

Download the HL-CRM rev. 2 geometry model from the workshop ftp site.

Right click on the file link and use Save link as.

Images