From 45523ae1cc23370bdd702e4472d648cc94e72770 Mon Sep 17 00:00:00 2001 From: Alvaro Cea Date: Fri, 3 Jan 2025 21:35:37 +0000 Subject: [PATCH] fix paths in README --- README.md | 26 +++++++++++++------------- 1 file changed, 13 insertions(+), 13 deletions(-) diff --git a/README.md b/README.md index 2bbad9b..4c9715f 100644 --- a/README.md +++ b/README.md @@ -78,7 +78,7 @@ The most relevant examples in the code base are shown here, these and more can b They are also part of a large test suite that is integrated into the development using CI/CD. !!! tip - Navigate to the code of the various examples, including the simulation input settings and postprocessing of the simulation --exactly as it was used for the articles backing the software. See [examples](./examples.md) + Navigate to the code of the various examples, including the simulation input settings and postprocessing of the simulation --exactly as it was used for the articles backing the software. See [examples](./docs/examples.md) ### Nonlinear structural static results @@ -87,9 +87,9 @@ They are also part of a large test suite that is integrated into the development - AD differentiation of the response verified against finite-differences -[Notebook](./examples/SailPlane/sailplane_nb.md) +[Notebook](./docs/examples/SailPlane/sailplane_nb.md) -![Sail Plane static](./img/SailPlane3D_front.png) +![Sail Plane static](./docs/img/SailPlane3D_front.png) !!! note Take a liner FE model of arbitrary complexity from your favourite FE solver, and turn it into a fully geometrically nonlinear model. You just need a condensation step into the main load paths and the resulting linear stiffness and mass matrices. @@ -99,22 +99,22 @@ They are also part of a large test suite that is integrated into the development - Runs over x100 faster than Nastran - AD differentiation of the response verified against finite-differences -[Notebook](./examples/wingSP/wingSP_nb.md) +[Notebook](./docs/examples/wingSP/wingSP_nb.md) -![Wing free dynamics](./media/wingSP_optimized.gif) +![Wing free dynamics](./docs/media/wingSP_optimized.gif) ### Free flying structure This example first appeared in the work of Juan Carlos Simo (see [Bio](https://mechanics.stanford.edu/simo)) , a pioneer in the field of computational structural mechanics and the -[Notebook](./examples/wingSP/wingSP_nb.md) +[Notebook](./docs/examples/wingSP/wingSP_nb.md) #### 2D dynamics -![Free flying structure 2D](./media/SimoFFB2D_optimized.gif) +![Free flying structure 2D](./docs/media/SimoFFB2D_optimized.gif) #### 3D dynamics -![Free flying structure 3D](./media/SimoFFB3D_optimized.gif) +![Free flying structure 3D](./docs/media/SimoFFB3D_optimized.gif) ### Concurrent aeroelastic simulations on ultra-high aspect ratio aircraft !!! success @@ -128,16 +128,16 @@ This example first appeared in the work of Juan Carlos Simo (see [Bio](https://m - Validation of concurrent solution - 300 modes in the solution, 8 different loading scenarios running in parallel each with 11 substeps, 24 seconds in total on A100 GPU -![In-plane](./media/BugDiscrete3_L0.gif) -![Out-of-plane](./media/BugDiscrete3_L2.gif) -![Torsion](./media/BugDiscrete3_L4.gif) +![In-plane](./docs/media/BugDiscrete3_L0.gif) +![Out-of-plane](./docs/media/BugDiscrete3_L2.gif) +![Torsion](./docs/media/BugDiscrete3_L4.gif) #### Aeroelastic equilibrium for varying AoA - Nonlinear effects: follower aerodynamic forces, geometric stiffening, wing shortening. - Steady manoeuvre varying flow conditions and AoA for a total 256 cases in 14 seconds. -![Manoeuvre](./img/BUGmonoeuvre3D.jpg) +![Manoeuvre](./docs/img/BUGmonoeuvre3D.jpg) #### Dynamic loads at large scale: gust envelopes @@ -146,4 +146,4 @@ This example first appeared in the work of Juan Carlos Simo (see [Bio](https://m - Rigid body modes included, rigid/elastic nonlinear couplings accounted for. - Load envelopes available from the simulation. -![Gust response](./media/BugGust1.gif) +![Gust response](./docs/media/BugGust1.gif)