We add a dynamic aeroelastic stability analysis to our parametric wing analysis, so that we can calculate critical flutter and divergence flight velocities. We extract mass and stiffness information from our CalculiX model and then solve a complex eigenvalue problem with the help of the Scipy sparse matrix library.
In this post, we take a brief look at steered-fibre composites and particularly RTS composites. What are they? Why do we want to use them? And how do we design with them?
We add a simple parametric aerodynamics model to calculate the aero loads on the wing and couple it with our CalculiX structures model using the preCICE library and python API.
Over the last 18 months the company’s focus has changed but the name and logo stayed the same…until now! DaptaBlade was founded 2 years ago to commercialise the Z-beam novel aerodynamic tailoring technology that Olivia developed during her PhD. Olivia was looking to apply that technology to wind turbines, UAV wings and propellers, making “DaptaBlade” …
In our first blog post we want to demystify the topic of optimisation in engineering.What is it? Why would we want to use it? What are the challenges for practicing engineers today? If you wanted to implement design optimisation, where should you start? What are the mistakes to avoid? Read on for answers to these …
Welcome to the daptablog! A series on engineering simulation, automation, and collaboration. Boldly going where no engineers have gone before! At Dapta our goal is to help engineers achieve their imagination and build a sustainable world. We’re looking for the tools and methods that enable you to integrate your simulation tools and collaborate with your …
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