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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
User Guide
Overview
Chapter 1 Background
Chapter 2 OpenFOAM
Chapter 3 OpenMDAO
Chapter 4 NACA0012 2D airfoil
Chapter 5 NACA0012 variations
Chapter 6 ADODG3 3D wing
Chapter 7 UAV propeller
Chapter 8 Cylinder unsteady
Chapter 9 Ramp FIML
Chapter 10 Aerostructural
Chapter 11 Aerothermal (CHT)
Developer Guide
Overview
Background
DAFoam Code Structure
Python Layer
OpenFOAM Layer
Add New Features
V&V
Verification - Overview
Verification - DASimpleFoam
Validation - Overview
Validation - RAE2822 airfoil
Misc
GUI
DAFoam publications
DAFoam doxygen
Workshops
Acknowledgement
NACA0012 variations - compressibility, multi-point, multi-cases
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Note:
This webpage is under construction.