meshql 2.0.0

query based meshing on top of GMSH

meshql

Query-based meshing on top of GMSH

About

meshql is a declarative, query-based tool for parametric mesh generation built on top of GMSH. It provides an intuitive API for creating structured and unstructured meshes with support for:

• Query-based selection: Use CadQuery-like selectors to target specific geometry entities
• Boundary layers: Automatic boundary layer generation for both 2D and 3D meshes
• Transfinite meshing: Automated structured meshing with intelligent edge/face grouping
• Physical groups: Easy boundary condition assignment with named groups
• Preprocessing: Advanced geometry splitting and partitioning for complex workflows
• Multiple formats: Export to GMSH, SU2, VTK, and other mesh formats
• Visualization: Built-in mesh and geometry visualization tools

Installation

Prerequisites

meshql requires GMSH and CadQuery. Install them first:

# Install GMSH (required)
conda install -c conda-forge gmsh python-gmsh

# Install CadQuery (required for CAD geometry support)
conda install -c conda-forge -c cadquery cadquery=master

From PyPI

pip install git+https://github.com/OpenOrion/meshql.git#egg=meshql

From Source

git clone https://github.com/OpenOrion/meshql.git
cd meshql
pip install -e ".[gmsh]"

Quick Start

Basic Example: NACA Airfoil with Boundary Layer

import cadquery as cq
from meshql import GeometryQL
from meshql.utils.shapes import generate_naca4_airfoil

# Generate NACA 0012 airfoil coordinates
airfoil_coords = generate_naca4_airfoil("0012", num_points=40)

with GeometryQL.gmsh() as geo:
    mesh = (
        geo
        .load(
            cq.Workplane("XY")
            .circle(20)
            .polyline(airfoil_coords)
            .close()
        )
        
        # Configure airfoil surface
        .edges(type="interior")
        .addPhysicalGroup("airfoil")
        .addBoundaryLayer(
            ratio=2,
            size=0.00001,
            num_layers=40,
        )
        .setMeshSize(0.01)
        .end()

        # Configure farfield
        .edges(type="exterior")
        .addPhysicalGroup("farfield")
        .setMeshSize(3.0)
        .end()

        .generate(2)
        .show("mesh")
    )

Structured Mesh with Preprocessing

import cadquery as cq
from meshql import GeometryQL, Split

with GeometryQL.gmsh() as geo:
    (
        geo
        .load(
            cq.Workplane("XY").box(10, 10, 10).rect(2, 2).cutThruAll(),
            preprocess=(Split, lambda split: (
                split
                .from_plane(angle=(90, 90, 0))
                .from_plane(angle=(-90, 90, 0))
            )),
        )
        .setTransfiniteAuto(max_nodes=50)
        .generate(3)
        .show("mesh", only_surface=True)
    )

3D Wing with Interior Faces

import cadquery as cq
import numpy as np
from meshql import GeometryQL
from meshql.utils.shapes import generate_naca4_airfoil

airfoil_coords = generate_naca4_airfoil("0012", num_points=40) * 5 - np.array([2.5, 0])

with GeometryQL.gmsh() as geo:
    (
        geo
        .load(
            cq.Workplane("XY")
            .box(10, 10, 10)
            .faces(">Z")
            .workplane(centerOption="CenterOfMass")
            .polyline(airfoil_coords)
            .close()
            .cutThruAll()
        )
        .faces(type="interior")
        .addPhysicalGroup("wing")
        .addBoundaryLayer(size=0.001, ratio=1.5, num_layers=3)
        .end()
        .generate(2)
        .show("mesh")
    )

Key Features

Selection System

Use intuitive CadQuery-style selectors to target geometry entities:

.faces(">Z")           # Top faces
.edges(type="interior") # Interior edges
.solids()              # All solids
.vertices()            # All vertices

Meshing Operations

Boundary Layers

Automatic boundary layer generation for viscous flow simulations:

.addBoundaryLayer(
    size=0.001,        # First cell height
    ratio=1.5,         # Growth ratio
    num_layers=10,     # Number of layers
)

Transfinite Meshing

Automated structured meshing with intelligent parameter selection:

.setTransfiniteAuto(
    max_nodes=50,           # Maximum nodes per edge
    min_nodes=2,            # Minimum nodes per edge
    auto_recombine=True,    # Recombine to quads/hexes
)

Physical Groups

Assign boundary conditions with named groups:

.faces(">Z")
.addPhysicalGroup("top_wall")
.end()

.faces("<Z")
.addPhysicalGroup("bottom_wall")
.end()

Mesh Refinement

Control mesh size and algorithms:

.setMeshSize(0.1)                     # Set mesh size
.setMeshAlgorithm2D("Delaunay")       # 2D algorithm
.setMeshAlgorithm3D("Delaunay")       # 3D algorithm
.refine()                             # Refine mesh
.recombine()                          # Recombine elements

Preprocessing

Geometry Splitting

Split complex geometries for structured meshing:

preprocess=(Split, lambda split: (
    split
    .from_plane(angle=(90, 90, 0))           # Split by plane
    .from_ratios([0.25, 0.5, 0.75])          # Split by ratios
    .from_normals([(1, 0, 0), (0, 1, 0)])    # Split by normals
    .from_edge(selector=">Z")                 # Split from edge
))

Mesh Import

Load existing meshes from various formats:

import meshly

mesh = meshly.Mesh(
    vertices=vertices_array,
    indices=indices_array,
    markers={"boundary": [face_indices]}
)

geo.load(mesh)

Output Formats

Export to multiple mesh formats:

.write("output.msh", dim=2)   # GMSH format
.write("output.su2", dim=2)   # SU2 format
.write("output.vtk", dim=2)   # VTK format

Visualization

Built-in visualization tools:

.show("mesh")                       # Show mesh
.show("mesh", only_surface=True)    # Show surface only
.show("gmsh")                       # Open in GMSH GUI

Examples

More examples available in the examples directory:

• cube.ipynb: Basic structured meshing with boundary layers
• naca0012.ipynb: Airfoil meshing with boundary layers
• inviscid_wedge.ipynb: Inviscid flow simulation setup
• turbo.ipynb: Turbomachinery example with STEP import
• progression.ipynb: Mesh refinement progression

Documentation

• Changelog: Version history and feature releases

Development Setup

Quick Start

git clone https://github.com/OpenOrion/meshql.git
cd meshql
make install

Available Make Commands

# Install package in development mode with GMSH support
make install

# Build Python package
make build-package

# Run tests
make test

# Clean build artifacts
make clean

# Quick local build (for testing)
make build

Manual Installation

git clone https://github.com/OpenOrion/meshql.git
cd meshql
pip install -e ".[gmsh]"

Contributing

We welcome contributions! Please check out the Discord for discussions and collaboration.

Support

• Discord: Join our community
• Issues: Report bugs or request features

Tutorial

Video tutorial available:

latest: https://www.youtube.com/watch?v=7skc6wjwoTk

v1: https://www.youtube.com/watch?v=ltbxRsuvaLw

License

MIT License - see LICENSE file for details.