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Copy file name to clipboardExpand all lines: README.md
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@@ -56,9 +56,10 @@ In Julia, first update the packages:
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using Pkg
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Pkg.update()
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```
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and then you can execute the first example:
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and then you can display a menu with the available examples:
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```julia
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include("examples/rectangular_wing.jl")
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using VortexStepMethod
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menu()
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```
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To browse the code, it is suggested to use [VSCode](https://code.visualstudio.com/) with the Julia plugin.
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"inviscid")
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# Step 3: Initialize aerodynamics
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wa =WingAerodynamics([wing])
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wa =BodyAerodynamics([wing])
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# Set inflow conditions
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vel_app = [cos(alpha), 0.0, sin(alpha)] .* v_a
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## Citation
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If you use this project in your research, please consider citing it.
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Citation details can be found in the [CITATION.cff](CITATION.cff) file included in this repository.
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Citation details can be found in the [CITATION.cff](https://github.com/Albatross-Kite-Transport/VortexStepMethod.jl/blob/main/CITATION.cff) file included in this repository.
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## License
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This project is licensed under the MIT License - see the [LICENSE](LICENSE) file for details.
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## WAIVER
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Technische Universiteit Delft hereby disclaims all copyright interest in the package “VortexStepMethod.jl” written by the Author(s).
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Prof.dr. H.G.C. (Henri) Werij, Dean of Aerospace Engineering
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### Copyright
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Copyright (c) 2022 Oriol Cayon
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Copyright (c) 2024 Oriol Cayon, Jelle Poland, TU Delft
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Copyright (c) 2025 Oriol Cayon, Jelle Poland, Bart van de Lint
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Copyright (c) 2025 Oriol Cayon, Jelle Poland, Bart van de Lint, Uwe Fechner
**AIC:** Aerodynamic Influence Coefficient (AIC). The AIC matrix represents the relationship between the induced velocities or pressures on aerodynamic surfaces and the circulation strength or modal deformations of the lifting surfaces.
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### References:
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[Fast Aero-Structural Model of a Leading-Edge Inflatable Kite](https://www.mdpi.com/1996-1073/16/7/3061) by Oriol Canon, Mac Gaunaa and Roland Schmehl, Energies 2023 16(7), doi: 10.3390/en16073061
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For extensions of the original work see: [News.md](https://github.com/Albatross-Kite-Transport/VortexStepMethod.jl/blob/main/NEWS.md).
Copy file name to clipboardExpand all lines: docs/src/index.md
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@@ -57,9 +57,10 @@ In Julia, first update the packages:
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using Pkg
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Pkg.update()
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```
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and then you can execute the first example:
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and then you can display a menu with the available examples:
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```julia
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include("examples/rectangular_wing.jl")
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using VortexStepMethod
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menu()
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```
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To browse the code, it is suggested to use [VSCode](https://code.visualstudio.com/) with the Julia plugin.
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@@ -105,7 +106,7 @@ add_section!(wing,
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"inviscid")
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# Step 3: Initialize aerodynamics
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wa =WingAerodynamics([wing])
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wa =BodyAerodynamics([wing])
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# Set inflow conditions
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vel_app = [cos(alpha), 0.0, sin(alpha)] .* v_a
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Citation details can be found in the [CITATION.cff](https://github.com/Albatross-Kite-Transport/VortexStepMethod.jl/blob/main/CITATION.cff) file included in this repository.
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## License
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This project is licensed under the MIT License - see the [LICENSE](https://github.com/Albatross-Kite-Transport/VortexStepMethod.jl/blob/main/LICENSE) file for details.
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This project is licensed under the MIT License - see the [LICENSE]((https://github.com/Albatross-Kite-Transport/VortexStepMethod.jl/blob/main/LICENSE) file for details.
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## WAIVER
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Technische Universiteit Delft hereby disclaims all copyright interest in the package “VortexStepMethod.jl” written by the Author(s).
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Prof.dr. H.G.C. (Henri) Werij, Dean of Aerospace Engineering
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### Copyright
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Copyright (c) 2022 Oriol Cayon
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Copyright (c) 2024 Oriol Cayon, Jelle Poland, TU Delft
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Copyright (c) 2025 Oriol Cayon, Jelle Poland, Bart van de Lint
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Copyright (c) 2025 Oriol Cayon, Jelle Poland, Bart van de Lint, Uwe Fechner
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