Impact modelling for narrowbody fan blades
Development of impact-modelling techniques for narrowbody fan blade applications, integrating numerical modelling with experimental results.
Royal Academy of Engineering Research Fellow · University of Oxford
I lead the Composites and Interface Mechanics themes at Oxford's Impact and Shock Mechanics Laboratory. My group measures how adhesive joints, fibre reinforced composites and 3D-printed materials fail when loaded in microseconds, and turns those measurements into models that partners such as Rolls-Royce design with.
Research programme
Modern aircraft, vehicles and protective equipment are built from heterogeneous materials: carbon-fibre laminates, adhesively bonded metal-to-composite joints, additively manufactured parts. Every one of them contains interfaces, and under bird strike, a crash or a blow to the head it is most commonly the interface that fails first. My Royal Academy of Engineering Fellowship, Unveiling Interface Dynamics: Empowering Structural Response in Extreme Environments, builds the experimental and computational tools to predict that failure across length scales and loading rates, so that lighter, more sustainable structures can be certified with confidence.
From quasi-static to shock
A fan-blade-off event loads material roughly a million times faster than a standard tensile test. Properties measured at one rate do not necessarily transfer to another, so my group characterises materials across a range of rates with the same specimen geometry, and builds models that hold at every point on it.
Where everyday events sit on the scale
Indicative ranges. Every experiment feeds a matching simulation: rate-, thickness-, temperature- and void-dependent cohesive zone laws implemented as user subroutines in Abaqus and LS-DYNA.
Titanium adherendbonded to
Bonded joints replace rivets and save weight, but their strength changes with loading rate, bondline thickness and temperature. I developed the methods that measure the full traction–separation response of aerospace adhesives from quasi-static to impact rates, linked the thickness effect to micro-voids seen in X-ray CT, and ran the first dynamic fracture experiments on carbon-fibre-to-titanium joints, which revealed that failure switches from the adhesive to the composite as the rate rises.
Engine casings must contain high-speed debris; fan blades must survive bird strike. At impact rates the load can't be reliably measured, so the delamination fracture energy is hard to determine. Using the load-free optical method I developed, and working with Rolls-Royce and Innovate UK, we showed that aerospace carbon-fibre laminates are 56–66% tougher against delamination at impact rates than in a standard quasi-static test, with fractography tracing the rise to a change in failure mechanism.
Additive manufacturing lets us design the interior of a material, not just its shape. We built a test method that impacts mouthguards at realistic field-hockey energies, rather than the far gentler standard, and showed that a 3D-printed design cut peak force by 10% and impulse by 25% against the thermoformed EVA benchmark. Internal air-cell structures dissipated a further 25% more energy, and a strain-rate material model ties the design back to how the polymer behaves at impact.
Real parts contain voids, impurities and process-induced variability. The next phase of the fellowship quantifies how designed and accidental heterogeneity combine to govern impact performance, through stochastic defect–property modelling, machine-learning crack detection from X-ray imaging, and vibration-based structural health monitoring of composite blades.
Gallery
Figures from open-access papers: synchrotron tomography of damage inside a laminate, strain fields around a moving crack, the rigs that load a specimen in microseconds, and the printed parts they test. Click any image to see it in full.
Damage inside a carbon-fibre laminate after high-rate compression, reconstructed from synchrotron X-ray tomography at the ESRF. Warm colours mark delamination and ply cracks; the rows compare room temperature with −50 °C. Sun et al., Composites Part A (2026)
Strain field from digital image correlation ahead of a delamination crack in a wedge-loaded specimen during a Hopkinson-bar test. Chen et al., Composites Part B (2023)
The modified direct-impact Hopkinson pressure bar developed for soft, low-impedance materials such as foams and printed lattices. Lee et al., International Journal of Impact Engineering (2026)
A 3D-printed mouthguard on its fixture ahead of drop-tower testing at field-hockey impact energies. Lißner et al., Materials & Design (2023)
Printed cellular designs for mouthguards, from CAD to printed part: solid, cubic air cells and spherical air cells. Saunders et al., Scientific Reports (2022)
Fracture surfaces of the same composite after quasi-static and high-rate delamination. The failure mechanism changes with loading speed. Chen et al., Composites Part B (2023)
Strain localising at grain boundaries in a nickel superalloy at 750 °C, measured in-situ in the electron microscope and reproduced by a crystal-plasticity model with cohesive boundaries. Alabort et al., Acta Materialia (2018)
A strain-gauged wedge entering a double-cantilever-beam specimen inside the Hopkinson bar, with the measured wedge velocity. Ponnusami et al., Composite Structures (2022)
Printed thermoplastic and standard EVA specimens before and after impacts at up to 10 m/s. Saunders et al., Scientific Reports (2022)
All figures are reproduced from articles published under the Creative Commons Attribution (CC BY) licence and are credited to their source papers.
Projects
Development of impact-modelling techniques for narrowbody fan blade applications, integrating numerical modelling with experimental results.
Improvement of impact-modelling techniques for composite containment casings, integrating numerical modelling with experimental results.
A five-year programme on interface failure in layered structures under dynamic conditions, developing a multiscale experimental–numerical workflow for interlaminar fracture and new additively manufactured specimen designs for interface characterisation.
Uniting dynamic-materials researchers across Mondragon University, the University of Rijeka and Arts et Métiers Bordeaux, and establishing educational programmes on the dynamic behaviour of materials. Project manager for the consortium.
International collaboration between TU Dresden, King's College London and the University of Oxford on the effect of space on human physiology.
Customised materials for protective systems through additive manufacturing. One of five fellows selected to build an independent research profile at the Institute of Lightweight Engineering and Polymer Technology.
Working with industry
Publications
Journal of the Mechanics and Physics of Solids, Acta Materialia, ACS Nano, Composites Part A and B, International Journal of Impact Engineering, Materials & Design and more. Full records on Google Scholar and ORCID.
Source: Google Scholar, retrieved 18 September 2026. 2026 is year to date.
Citations per year
Click any card to read the abstract. Names in bold mark Maria Lißner's authorship. One further manuscript on topology optimisation with stress-state-dependent damage is under review.
Recognition
The Association of German Engineers' award for engineers under 40 whose work stands out far beyond the ordinary, presented in Düsseldorf for interdisciplinary contributions to lightweight structures under extreme loading. Oxford news · VDI interview
Five years of support for an integrated programme on interface characteristics across multiple length scales in heterogeneous materials under extreme loading. Oxford news · RAEng profile
For leading industry projects, supervising researchers and collaborating with Rolls-Royce plc and Innovate UK.
Europe's dynamic-behaviour-of-materials association recognised the thesis Characterisation and modelling of the rate-dependent behaviour of adhesively bonded interfaces for the excellence and scale of its research. Oxford news
One of five fellows selected by TU Dresden to build an independent research programme. TU Dresden
Co-founded the Oxford X-Reality Hub, connecting immersive-technology researchers across the University, and taught over 400 hours of augmented and virtual reality courses.
Leadership, teaching and community
Selected invited talks
Collaborate
I welcome conversations with industrial partners who need rate-dependent data and models they can design with, funders looking to support interface mechanics for safer and more sustainable structures, and researchers interested in joint proposals, visits or co-supervised students.