diff --git a/README.md b/README.md index 846dbb4..ec0fa36 100644 --- a/README.md +++ b/README.md @@ -25,12 +25,16 @@ - [Table of Contents](#table-of-contents) - [Introduction](#introduction) - [Features](#features) + - [Screenshots](#screenshots) - [Installation](#installation) - [Prerequisites](#prerequisites) - - [Steps](#steps) - - [Windows Executable (Windows 11 an 10)](#windows-executable-windows-11-an-10) - - [License](#license) + - [Option 1: Windows Executable (Windows 10/11)](#option-1-windows-executable-windows-1011) + - [Option 2: Install from Source](#option-2-install-from-source) + - [Usage](#usage) + - [Project Structure](#project-structure) - [Submitting Issues](#submitting-issues) + - [License](#license) + - [Author](#author) - [Acknowledgements](#acknowledgements) --- @@ -43,52 +47,115 @@ ## Features -- Compute aerodynamic coefficients ($C_L$, $C_D$, moments) for various wing configurations. -- Interactive 2D/3D visualization with Plotly. -- Customizable wing geometry: sweep, dihedral, taper, control surfaces. -- Analyze multiple flight conditions (angle of attack, sideslip, airspeed). -- NACA airfoil generation and analysis. -- Modular, extensible Python architecture. +- **Accurate VLM Implementation**: Compute aerodynamic coefficients ($C_L$, $C_D$, moments) for wing configurations. +- **Interactive Visualization**: 2D/3D plots of lift distribution, pressure coefficients, and geometry using Plotly and Matplotlib. +- **Customizable Geometry**: Define wing parameters like sweep, dihedral, taper, and control surfaces. +- **Flexible Flight Conditions**: Analyze multiple angles of attack, sideslip angles, and airspeeds. +- **NACA Airfoil Support**: Generate and analyze NACA airfoil profiles. +- **Modular Architecture**: Extensible Python codebase for custom analyses and integration with NumPy, Matplotlib, and more. +- **User-Friendly Interface**: Intuitive Python API, ready-to-use executables, and Jupyter notebook examples. +- **Comprehensive Documentation**: Step-by-step guides and practical examples. --- +### Screenshots + +
+ +| ![Welcome](docs/screenshots/APP/bienvenida.png) | ![Main Menu](docs/screenshots/APP/menu.png) | +|:--:|:--:| +| Welcome | Main Menu | + +| ![Curvature](docs/screenshots/APP/curvatura.png) | ![3D Discretization](docs/screenshots/A320/Wing_Discretization3d_htpyvtp1.svg) | +|:--:|:--:| +| Wing Curvature | 3D Wing Discretization (A320) | + +
+ +
+View all screenshots + +- **Welcome** + ![Welcome](docs/screenshots/APP/bienvenida.png) + +- **Main Menu** + ![Main Menu](docs/screenshots/APP/menu.png) + +- **Wing Curvature** + ![Curvature](docs/screenshots/APP/curvatura.png) + +- **3D Wing Discretization (A320)** + ![3D Discretization](docs/screenshots/A320/Wing_Discretization3d_htpyvtp1.svg) + +- **Vorticity Distribution (Flat Plate with Aileron)** + ![Gammas](docs/screenshots/Placa%20plana%20con%20aleron/Gammas.svg) + +
## Installation ### Prerequisites -- Python 3.8+ -- Web browser (Chrome 90+, Firefox 85+, or equivalent) +- **Python 3.8+** (for source installation) +- **Web Browser** (Chrome 90+, Firefox 85+, or equivalent) +- **Git** (optional, for cloning the repository) +- +### Option 1: Windows Executable (Windows 10/11) -### Steps +1. Download `app.exe` from the [Releases page](https://github.com/JaviLendi/VLMPy/releases). +2. Double-click to launch the application—no additional setup required. + +### Option 2: Install from Source 1. Clone the repository: - ```bash - git clone https://github.com/JaviLendi/VLMPy.git - cd VLMPy - ``` + ```bash + git clone https://github.com/JaviLendi/VLMPy.git + cd VLMPy + ``` 2. Install dependencies: - ```bash - pip install -r requirements.txt - ``` - *Tip*: Update pip with `pip install --upgrade pip` if needed. + ```bash + pip install -r requirements.txt + ``` + *Tip*: Update pip with `pip install --upgrade pip` if needed. 3. Run the app: - ```bash - python app.py - ``` - Access at [http://localhost:5000](http://localhost:5000). + ```bash + python app.py + ``` +4. Access the web interface at [http://localhost:5000](http://localhost:5000). -#### Windows Executable (Windows 11 an 10) +--- +## Usage -Download `app.exe` from the [Releases page](https://github.com/JaviLendi/VLMPy/releases) and double-click to launch. +- **Executable**: Launch `app.exe` (Windows) for a standalone experience. +- **Python API**: Import VLMPy modules in your scripts for custom analyses (see `src/lib/`). +- **Jupyter Notebooks**: Explore example notebooks in the `notebooks/` directory for guided tutorials. +- **Web Interface**: Run `app.py` to access the interactive web app at [http://localhost:5000](http://localhost:5000). ---- +Example scripts and documentation are available in the `notebooks/` and `docs/` directories. -## License +--- -VLMPy is distributed under the [GNU Affero General Public License v3.0 (AGPL-3.0)](LICENSE). +## Project Structure + +``` +VLMPy/ +├── src/ # Source code +│ ├── lib/ # Core VLM and utility modules +│ │ ├── vlm.py # Vortex Lattice Method implementation +│ │ ├── naca.py # NACA airfoil generation utilities +│ │ ├── geometry.py # Wing geometry creation and manipulation +│ ├── static/ # Static assets (images, data files) +│ ├── templates/ # HTML templates for web interface +│ └── app.py # Application entry point +├── notebooks/ # Example Jupyter notebooks +├── docs/ # Documentation and project reports +├── requirements.txt # Python dependencies +├── README.md # Project documentation +└── LICENSE # License information +``` --- + ## Submitting Issues Found a bug or have a suggestion? Please open an issue on GitHub. @@ -101,11 +168,31 @@ Your feedback helps improve VLMPy! --- +## License + +VLMPy is distributed under the [GNU Affero General Public License v3.0 (AGPL-3.0)](LICENSE). + +--- + +## Author + +**Javier Lendínez Castillo** +_Aerospace Engineer_ + +- 💼 GitHub: [@JaviLendi](https://github.com/JaviLendi) +- 🏫 Universidad Alfonso X el Sabio + +--- + + ## Acknowledgements -- **Author:** Javier Lendínez Castillo -- **Supervisor:** Héctor Gómez Cedenilla -- **Date:** June 2025 +- **Supervisor**: Héctor Gómez Cedenilla +- **Institution**: Universidad Alfonso X el Sabio +- **Date**: June 2025 + +- **Additional Acknowledgements**: Marcos Antonio Rodríguez and Ignacio Maroto Villar, professors at Universidad Alfonso X el Sabio > ℹ️ For academic details and mathematical derivations, see `docs/TFG.pdf` (coming soon) and source code appendices. +--- \ No newline at end of file diff --git a/cache_plane_variables.txt b/cache_plane_variables.txt new file mode 100644 index 0000000..8c83b01 --- /dev/null +++ b/cache_plane_variables.txt @@ -0,0 +1,2 @@ +wing_sections: [{'chord_root': 1.0, 'chord_tip': 1.0, 'span_fraction': 8.0, 'sweep': np.float64(0.5235987755982988), 'alpha': np.float64(0.05235987755982989), 'dihedral': np.float64(0.06981317007977318), 'NACA_root': '3215', 'NACA_tip': '1310'}] +horizontal_stabilizer: {'x_translate': 2.0, 'z_translate': 0.0, 'NACA_root': '3215', 'NACA_tip': '3215', 'chord_root': 0.5, 'chord_tip': 0.5, 'span_fraction': 2.0, 'sweep': np.float64(0.5235987755982988), 'alpha': np.float64(0.0), 'dihedral': np.float64(0.0)} diff --git a/docs/DOCS.md b/docs/README.md similarity index 100% rename from docs/DOCS.md rename to docs/README.md diff --git a/docs/img/Github_social.png b/docs/img/Github_social.png new file mode 100644 index 0000000..ba5fef5 Binary files /dev/null and b/docs/img/Github_social.png differ diff --git a/docs/img/Github_social.svg b/docs/img/Github_social.svg new file mode 100644 index 0000000..ddeac10 --- /dev/null +++ b/docs/img/Github_social.svg @@ -0,0 +1,2306 @@ + + + +VLMPyA Vortex Lattice Method appOpen-source Python toolkit and application for aerodynamic analysis of wings using VLM. It makes it easy to model, visualize, and analyze lift and drag for a wide range of wing configurations in subsonic, inviscid flow. diff --git a/docs/screenshots/A320/Wing_Discretization2d (13).svg b/docs/screenshots/A320/Wing_Discretization2d (13).svg new file mode 100644 index 0000000..309e78c --- /dev/null +++ b/docs/screenshots/A320/Wing_Discretization2d (13).svg @@ -0,0 +1 @@ +−20−15−10−505101520−505101520Panel edgesControl points1/4 Chord linesWing Discretization - 2D Projectionsy [m]x [m]XY Projection▼ \ No newline at end of file diff --git a/docs/screenshots/A320/Wing_Discretization2d_2.svg b/docs/screenshots/A320/Wing_Discretization2d_2.svg new file mode 100644 index 0000000..3a5803a --- /dev/null +++ b/docs/screenshots/A320/Wing_Discretization2d_2.svg @@ -0,0 +1 @@ +−20−15−10−505101520−10−5051015Panel edgesControl points1/4 Chord linesWing Discretization - 2D ProjectionsXZ Projection▼ \ No newline at end of file diff --git a/docs/screenshots/A320/Wing_Discretization3d.svg b/docs/screenshots/A320/Wing_Discretization3d.svg new file mode 100644 index 0000000..9595963 --- /dev/null +++ b/docs/screenshots/A320/Wing_Discretization3d.svg @@ -0,0 +1 @@ +Panel edgesControl points1/4 Chord linesNormal vectorWing DiscretizationToggle normals and control points \ No newline at end of file diff --git a/docs/screenshots/A320/Wing_Discretization3d_1.svg b/docs/screenshots/A320/Wing_Discretization3d_1.svg new file mode 100644 index 0000000..e704139 --- /dev/null +++ b/docs/screenshots/A320/Wing_Discretization3d_1.svg @@ -0,0 +1 @@ +Panel edgesWing DiscretizationToggle normals and control points \ No newline at end of file diff --git a/docs/screenshots/A320/Wing_Discretization3d_htpvtp.svg b/docs/screenshots/A320/Wing_Discretization3d_htpvtp.svg new file mode 100644 index 0000000..7b9b683 --- /dev/null +++ b/docs/screenshots/A320/Wing_Discretization3d_htpvtp.svg @@ -0,0 +1 @@ +Panel edgesWing DiscretizationToggle normals and control points \ No newline at end of file diff --git a/docs/screenshots/A320/Wing_Discretization3d_htpyvtp1.png b/docs/screenshots/A320/Wing_Discretization3d_htpyvtp1.png new file mode 100644 index 0000000..165de8f Binary files /dev/null and b/docs/screenshots/A320/Wing_Discretization3d_htpyvtp1.png differ diff --git a/docs/screenshots/A320/Wing_Discretization3d_htpyvtp1.svg b/docs/screenshots/A320/Wing_Discretization3d_htpyvtp1.svg new file mode 100644 index 0000000..f148e39 --- /dev/null +++ b/docs/screenshots/A320/Wing_Discretization3d_htpyvtp1.svg @@ -0,0 +1 @@ +Panel edgesControl points1/4 Chord linesNormal vectorWing DiscretizationToggle normals and control points \ No newline at end of file diff --git a/docs/screenshots/A320/Wing_Geometry_2d.svg b/docs/screenshots/A320/Wing_Geometry_2d.svg new file mode 100644 index 0000000..e9a8817 --- /dev/null +++ b/docs/screenshots/A320/Wing_Geometry_2d.svg @@ -0,0 +1 @@ +−15−10−5051015−505101520Borde de ataqueBorde de salidaCuerda 1/4Geometría del ala (2D)y [m]x [m] \ No newline at end of file diff --git a/docs/screenshots/A320/Wing_Geometry_2d_con_htpyvtp.svg b/docs/screenshots/A320/Wing_Geometry_2d_con_htpyvtp.svg new file mode 100644 index 0000000..fbdf45f --- /dev/null +++ b/docs/screenshots/A320/Wing_Geometry_2d_con_htpyvtp.svg @@ -0,0 +1 @@ +−15−10−50510150510152025Borde de ataqueBorde de salidaCuerda 1/4Geometría del ala (2D)y [m]x [m] \ No newline at end of file diff --git a/docs/screenshots/A320/Wing_Geometry_2d_con_htpyvtp_discretizacion.svg b/docs/screenshots/A320/Wing_Geometry_2d_con_htpyvtp_discretizacion.svg new file mode 100644 index 0000000..e44207e --- /dev/null +++ b/docs/screenshots/A320/Wing_Geometry_2d_con_htpyvtp_discretizacion.svg @@ -0,0 +1 @@ +−20−15−10−5051015200510152025Panel edgesControl points1/4 Chord linesWing Discretization - 2D Projectionsy [m]x [m]XY Projection▼ \ No newline at end of file diff --git a/docs/screenshots/A320/Wing_Geometry_htpvtp.svg b/docs/screenshots/A320/Wing_Geometry_htpvtp.svg new file mode 100644 index 0000000..75633f9 --- /dev/null +++ b/docs/screenshots/A320/Wing_Geometry_htpvtp.svg @@ -0,0 +1 @@ +Borde de ataqueBorde de salidaCuerda 1/4Geometría del ala \ No newline at end of file diff --git a/docs/screenshots/APP/bienvenida.png b/docs/screenshots/APP/bienvenida.png new file mode 100644 index 0000000..6922872 Binary files /dev/null and b/docs/screenshots/APP/bienvenida.png differ diff --git a/docs/screenshots/APP/curvatura.png b/docs/screenshots/APP/curvatura.png new file mode 100644 index 0000000..440749a Binary files /dev/null and b/docs/screenshots/APP/curvatura.png differ diff --git a/docs/screenshots/APP/discretizacion2.png b/docs/screenshots/APP/discretizacion2.png new file mode 100644 index 0000000..ffb5855 Binary files /dev/null and b/docs/screenshots/APP/discretizacion2.png differ diff --git a/docs/screenshots/APP/menu.png b/docs/screenshots/APP/menu.png new file mode 100644 index 0000000..a4d481d Binary files /dev/null and b/docs/screenshots/APP/menu.png differ diff 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file mode 100644 index 0000000..bdf93dd --- /dev/null +++ b/docs/screenshots/Curvatura del ala/Curvature.svg @@ -0,0 +1 @@ +−4−2024−3−2−101234−0.015−0.01−0.00500.0050.01Curvature [1/m]Curvature DistributionX [m]Y [m] \ No newline at end of file diff --git a/docs/screenshots/Curvatura del ala/Gammas.pdf b/docs/screenshots/Curvatura del ala/Gammas.pdf new file mode 100644 index 0000000..9d78393 Binary files /dev/null and b/docs/screenshots/Curvatura del ala/Gammas.pdf differ diff --git a/docs/screenshots/Curvatura del ala/Gammas.svg b/docs/screenshots/Curvatura del ala/Gammas.svg new file mode 100644 index 0000000..36ae3c2 --- /dev/null +++ b/docs/screenshots/Curvatura del ala/Gammas.svg @@ -0,0 +1 @@ +−4−2024−3−2−10123400.511.52Gamma [m²/s]Gamma DistributionX [m]Y [m] \ No newline at end of file diff --git a/docs/screenshots/Curvatura del ala/Geometria-XFLR5.png b/docs/screenshots/Curvatura del ala/Geometria-XFLR5.png new file mode 100644 index 0000000..c04fb05 Binary files /dev/null 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b/docs/screenshots/Placa plana con aleron/Wing_Geometry_2d.pdf differ diff --git a/docs/screenshots/Placa plana con aleron/Wing_Geometry_2d.svg b/docs/screenshots/Placa plana con aleron/Wing_Geometry_2d.svg new file mode 100644 index 0000000..45d2b20 --- /dev/null +++ b/docs/screenshots/Placa plana con aleron/Wing_Geometry_2d.svg @@ -0,0 +1 @@ +−4−2024−2−10123Borde de ataqueBorde de salidaCuerda 1/4Geometría del ala (2D)y [m]x [m] \ No newline at end of file diff --git a/docs/screenshots/Placa plana con flap/CL-XFLR5.png b/docs/screenshots/Placa plana con flap/CL-XFLR5.png new file mode 100644 index 0000000..ff1a1fb Binary files /dev/null and b/docs/screenshots/Placa plana con flap/CL-XFLR5.png differ diff --git a/docs/screenshots/Placa plana con flap/CL-alpha.svg b/docs/screenshots/Placa plana con flap/CL-alpha.svg new file mode 100644 index 0000000..5e42c37 --- /dev/null +++ b/docs/screenshots/Placa plana con flap/CL-alpha.svg @@ -0,0 +1 @@ +02468100.60.811.21.4CLLift Coefficient vs 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