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Documentation v4.0.2
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Overview
Download docker image
Run optimization
Post-processing
Details of run scripts
FAQ
Installation
Compile from source (Ubuntu)
Compile from source (HPC)
Build a new Docker image
Tutorials
Overview
Aerodynamics
NACA0012 airfoil (low speed)
NACA0012 airfoil (subsonic)
NACA0012 airfoil (transonic)
NACA0012 airfoil (multipoint)
Cylinder (unsteady flow)
30N30P multi-element airfoil
Onera M6 wing
ADODG3 wing
CRM wing
Prowim wing propeller
DPW4 aircraft
Rotor37 compressor
NREL6 wind turbine
Aerostructural
MACH tutorial wing
UAV propeller
Aerothermal
U-bend channel
U-bend pipe CHT
Solid mechanics
Plate hole
Hydrodynamics
JBC hull
Topology optimization
pitzDaily
Field inversion ML
Periodic hill
Ramp
GUI
Overview
Mesh Generation
Airfoil optimization
Post Processing
User Guide
Overview
Chapter 1 Background
Chapter 2 OpenFOAM and DAFoam
Chapter 3 NACA0012 2D airfoil
Chapter 4 NACA0012 variations
Chapter 5 ADODG3 3D wing
Chapter 6 UAV propeller
Chapter 7 Cylinder unsteady
Chapter 8 Ramp FIML
Chapter 9 Aerostructural
Chapter 10 Aerothermal (CHT)
Developer Guide
Overview
V&V
Verification - Overview
Verification - DASimpleFoam
Validation - Overview
Validation - RAE2822 airfoil
Documents
DAFoam publications
DAFoam doxygen
Workshops
OpenFOAM and DAFoam Basics
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Note:
This webpage is under construction.
1. OpenFOAM
1.1 subsection