Doing More with Less: Pushing the frontiers of maximum strength with minimum weight.
Thursday, August 24, 2023 | Zoom Meeting Online 6:00 to 7:00 pm Pacific

Jens Bold, Boeing Research & Technology Europe, Munich
For decades, classical laminate theory has used linear material models to calculate stress in layered composite parts and then predict the structural load-carrying performance using a relatively simple failure criterion.
Now, modern non-linear material models and applying modal based failure criteria can lead to better predictions of structural load-carrying performance. The resulting optimization gains—delivering the required strength with less material and weight—yield a lower CO2 footprint in initial production, plus lower fuel cost and CO2 in ongoing operation.
In his online presentation, Jens Bold of Boeing Research & Technology Europe in Munich will take us through:
- The classical laminate theory methods,
- Newer validated methods to extract stress-strain curves as input for an advanced material model,
- Advanced modal based failure criteria for unidirectional and woven materials,
- Numerical methods with progressive failure analysis will be compared to standard linear methods for different types of numerical elements, such as 2D shell, 3D layered solid and 3D solid for each laminate layer,
- Validation for different element type specimens, including open- and filled-hole tension and compression, as well as compression after impact, and
- A comparison of the classical linear method using standard failure criteria with the advanced methods using non-linear material behavior and modal based failure criteria.
Join us at 6:00 pm PDT Thursday August 24th to explore the frontiers of composite simulation that are being pushed back in the never-ending tradeoff between structural strength and structural weight.
About Jens
Following his initial training in aerospace engineering at Technische Universität in Munich, Jens Bold worked in automotive engineering companies in Munich, then moved into aerospace at Eurocopter in helicopter and aircraft doors development.
He then moved to Airbus working on fuselage and fin stress, with responsibility for 110 employees in three countries, and organizing worldwide composite training inside Airbus. In 2008 he moved back into automotive, joining the Toyota F1 team in Cologne. From there back to aerospace (and back to school) working with DLR (German Center for Air and Space Flight) aircraft wing design projects and starting his PhD thesis. He was then manager of new composites technologies at Johnson Controls, and later joined Boeing Research & Technology Europe in the new office in Munich in February 2016.
Jens received his doctorate in engineering in 2019, with thesis focused on developing the Cuntze-Bold failure and material model for composites. Since 2023 the Cuntze-Bold non-linear material model combined with Cuntze modal based failure criteria has been embedded in core MSC Nastran as MATCB (Cuntze-Bold). He is inventor or co-inventor on 28 patent filings relating to doors, windows, seats, fuselage beams, component joints and continuous fabrication methods.
Registration
There’s no charge to attend, If you register in advance, we’ll send you the calendar meeting invitation with all the Zoom connection options. Click the button to register:
If you don’t want to register in advance, please feel free to put it in your calendar to join us using this Zoom link: MEETING LINK Meeting ID: 858 1794 9201 Passcode: 520632