MESH ADAPTATION FOR RANS TFG
5th
AIAA CFD High Lift Prediction Workshop
Page under construction
The ADAPT Technology Focus Group (TFG) facilitates the development and use of automated mesh adaptation
techniques and strategies. Although primarily concerned with Reynolds-averaged Navier Stokes (RANS), it is also
open to exploring adaptive strategies for scale-resolving simulations. ADAPT TFG objectives include producing
grid-converged verified solutions for a given model and understanding how these verified solutions compare
to experimental data.
The following lists the active membership for this Technology Focus Group (TFG).
The assigned Participant ID (PID) numbers are given in red.
(The PIDs may not be contiguous or in numerical order, as teams may drop out or be added.)
Please contact
hiliftpw@gmail.com
if you have a correction.
Mesh Adaptation (meshing and CFD)
TFG Leader
Members
- A-001 (KTH):
- Johan Jansson (also in WMLES TFG)
- Kristoffer Wingstedt
- Rebecca Durst
- A-002 (Istanbul Technical University):
- A-003 (Boeing):
- A-004 (INRIA):
- A-005 (MIT):
- Marshall Galbraith (also in HO TFG)
- A-006 (Ansys):
- A-007 (Politecnico Milan):
Key Questions
- Can adaptive mesh convergence be achieved on the CRM-HL Wing-Body to verify implementations?
- Can adaptive mesh refinement identify consistent trends due to increasing geometric complexity across the angle of attack range?
- Can adaptive mesh refinement resolve Reynolds number trends in integrated forces, moment, and separation patterns across the angle of attack range?
- Where can mesh adapted RANS contribute to prediction of high-lift flow physics?
Return to: TFG List and Associated Documents Top Page
Return to: High Lift Prediction Workshop Home Page
Recent significant updates:
04/09/2024 - added A-007 team
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Responsible NASA Official:
Christopher Rumsey
Page Curator:
Christopher Rumsey
Last Updated: 04/09/2024