mdolab MACH-Aero · Discussions · GitHub

Discussions

You must be logged in to vote

What is the difference between DAfoam and MACH-aero?

haizhou0410 started Jun 11, 2025 in General

0
You must be logged in to vote

Problem with extrusion of surface mesh of DLR F6 wing body using pyhyp

hassanakbar82 asked May 22, 2025 in Q&A · Closed · Unanswered

1
You must be logged in to vote

Maximum deviation warning in tutorial

TufanAkba started May 13, 2025 in General

0
You must be logged in to vote

Running Apptainer images on HPC

orliac started Oct 1, 2024 in General

9
You must be logged in to vote

Meshing generation to add a ground on a vehicle CFD analysis

cggailla asked Oct 11, 2024 in Q&A · Unanswered

1
You must be logged in to vote

Geometrically Nonlinear High-fidelity Aerostructural Optimization

Aming12-01 started Aug 20, 2024 in General

0
You must be logged in to vote

Extract optimized 3d geometry for CAD software

umarsajjad1992 started Jul 23, 2024 in Ideas · Closed

3
You must be logged in to vote

Problem with Aerostructural optimzation of wing

Aming12-01 started Jul 4, 2024 in General

0
You must be logged in to vote

Probelm with Mphys in docker image

Aming12-01 asked Jun 13, 2024 in Q&A · Closed · Answered

2
You must be logged in to vote

Confusion about system of units being used for flow conditions and geometry in ADFLOW

umarsajjad1992 asked Jun 13, 2024 in Q&A · Unanswered

0
You must be logged in to vote

maximization lift coefficient for an the objective function for multiple point airfoil optimization

EngJamal2023 asked Dec 7, 2023 in Q&A · Unanswered

1
You must be logged in to vote

new beginner how i could change the option of the SLSQP like the other optimizer

MachAeroDeveloper started Jan 27, 2024 in General · Closed

1
You must be logged in to vote

failure mesh output when i do single point optimization for airfoil shape optimization for

MachAeroDeveloper started Jun 12, 2024 in General

0
You must be logged in to vote

Different geometric design variables in multi-point optimization

MYH-student started May 10, 2024 in General

1
You must be logged in to vote

aero_opt.py: Cannot add leading edge constraints. The dimensions of the selected face are: (2, 2). For this case you must specify topID

yangchas asked May 13, 2024 in Q&A · Unanswered

1
You must be logged in to vote

Saving the Optimized FFD box

AbhijithMoni asked Apr 22, 2024 in Q&A · Closed · Unanswered

0
You must be logged in to vote

Questions on cgns grid file; which is to be read and solved using ADFLOW

vaths1 asked Apr 4, 2024 in Q&A · Unanswered

1
You must be logged in to vote

Mesh Parameterization for specified surfaces

AbhijithMoni asked Mar 20, 2024 in Q&A · Closed · Answered

6
You must be logged in to vote

Trying to Run different airfoil (Naca0018) Instead of the airfoilopt(Naca0012)

vaths1 asked Mar 16, 2024 in Q&A · Answered

2
You must be logged in to vote

single point optimization failed to do the optimization seeking for help in this issues

MachAeroDeveloper started Jan 25, 2024 in General

0
You must be logged in to vote

Saving the Mesh after Parametrization

AbhijithMoni asked Dec 4, 2023 in Q&A · Closed · Answered

4
You must be logged in to vote

Very beginner user. Problems running container in Docker

agusbuffa asked Jan 12, 2024 in Q&A · Answered

2
You must be logged in to vote

failed optimization at low mach number 0.044 at maximization lift for single point optimization for same tutorial NACA0012

EngJamal2023 asked Nov 12, 2023 in Q&A · Answered

2
You must be logged in to vote

bugs the simulation is not stop to do simulation for single point optimization and not terminated succussfully for SLSQP optimizer

EngJamal2023 started Nov 19, 2023 in General

0
You must be logged in to vote

how do I build the shell script?

haizhou0410 asked Nov 16, 2023 in Q&A · Unanswered

2