Analysis/Simulation

Analytic sizing

We believe that for most composite structures it is beneficial to perform an analytic sizing hand in hand with the design prior to FEM calculation. This improves understanding and simplification of load paths and yields a fiber-appropriate and cost-effective design. Analytic sizing is done using Jupyter Notebooks in conjuncture with git to allow version control. We have an extensive code base which we adjust rapidly to fulfill your needs.

We perform:

  • Analytic structural strength calculation according to engineering standards
  • Analytic static stability analysis (buckling)
  • Composite fatigue analyis (linear fatigue accumulation)
Analytic sizing
Dimensions and stresses of a CFRP sparcap, the main load carrying structure in an aircraft wing.

FEM

After a detailed analytic sizing we use Finite Element Methods (FEM) to optimize your geometry and composite layup. Based on our extensive knowledge from academic research and industry projects, we optimize your structure to be as light as possible and structurally strong and stable. Based on the problem, we have proprietary and Open Source solvers available.

Depending on your needs, we perform:

  • Static & dynamic analyses
  • Buckling & modal analysis
  • Linear or nonlinear simulations
  • Numerical layup optimization
  • Topology optimization
FEM
FEM analysis of a 4-point bending test.

Topology Optimization

Our topology optimization software CMTop is capable of generating robust compliant mechanisms for motion and deformation control. It incorporates stress constraints, robust design with respect to manufacturing uncertainties and various objective functions (Force Inverter, Path generation, Compliance minimization). A nonlinear finite element solver, the latest filter and projection methods and stress constraints are featured. Furthermore, manufacturing uncertainties can be considered during optimization.

In the project MILAN, the software has been used to generate compliant mechanism stacks for the precise deformation of a morphing wing leading edge. But many other applications are conceivable – like Micro-Electro-Mechanical Systems (MEMS), robots, packaging and medical devices.

CMTop compliant mechanism
Compliant mechanism topology optimization.

Structural testing

We assist you with planning your structural testing campaign. Our experience spans the full testing pyramid – from small scale coupon tests over subcomponent tests to full scale structures. We already performed static breaking tests and a dynamic crash test of aircraft structures.

Structural testing Akaflieg Mue 31 Bruchversuch
Structural testing Akaflieg Mue 31 breaking test.

Johannes was responsible for planning, performing and analyzing the ultimate load test of the Mü-31 sailplane wing.

© Uli Benz, TU München