Members of the Steering Committee celebrate the start of a 5 year collaboration.

Members of the Steering Committee celebrate the start of a 5 year collaboration.

Members of the Steering Committee celebrate the start of a 5 year collaboration.

Members of the Steering Committee celebrate the start of a 5 year collaboration.

 Online COMAC-Imperial Research Centre Technical Workshop

The workshop was hosted on Monday 29th March 2021, via Microsoft Teams. Attendees included Centre Co-Directors, researchers, and their academic supervisors. The aim of the workshop was to provide an update on all active projects, but also to consider how those individual projects and research themes fit into the research centre as a whole. Presentation summaries can be found below.

Thermoplastic composites; thermoforming, impact, and repairby Richard Brooks, PhD Student

oneWe discussed the improved impact performance of thermoplastic composites compared to thermoset composites. We presented results from impact testing of repaired CF/Epoxy samples and plans for impact testing of repaired CF/PEEK samples. We then covered main findings from literature review into stamp forming, including frictional behaviour of material and the effect of processing parameters on final part quality. Our plans for pull-out test on CF/PPS to characterise inter-ply frictional behaviour and suitable forming conditions were also explained. The presentation was concluded by highlighted plans for impact testing of pristine and formed CF/PPS to investigate effect of forming on impact performance of the material.



High‐fidelity modeling of laminar flow transition to turbulenceby Ganlin Lyu, PhD Student

twoWe employ the eN method to predict laminar flow transition to turbulence at transonic flow condition and with the presence of surface roughness. The first step in the workflow is to obtain a flow field using a more efficient low-fidelity tool, such as RANS. Next, the baseflow in a smaller domain covering the target surface is computed, where the boundary conditions are interpolated from the flow field in the first step. Different profiles of the baseflow are analyzed to find out the most dangerous instabilities, whose developments along the surface are then simulated using the linearized Navier-Strokes solver. Finally, by post-processing the results, the envelope for the amplification curves of the instabilities are generated to get the N-factor, with which the flow transition can be predicted.

Dynamics of flexible aircraftby Stefanie Duessler, PhD Student


The computational methods we have been using for the GLA project are based on the open-source aeroelastic simulation environment SHARPy (, which is currently developed in our research lab. SHARPy couples unsteady aerodynamics with nonlinear structural dynamics. SHARPy can perform dynamic time-domain simulations of an aeroelastic system and access flexible-multibody vehicle dynamics to predict vehicle response. These capabilities are essential to accurately capturing the flight dynamic and rigid-body effects, necessary to explore new potential GLA strategies for next-generation commercial aircraft.

Progressive damage analysis in composite structures – by Dr Jun Liu


The aim of the project is to study in detail the delamination and dis-bond which may occur from impact on composite structures by various foreign objects e.g. hailstones or birds. With the use of experimental and numerical techniques, we are investigating the response of flat composite panels and patched repair composite structures against low velocity single- and multi-impact.


Creep age forming of AA2060 panels—experimental investigations on microstructural evolution of AA2060 during CAFby Xi Wang, PhD Student


The investigations of microstructural evolutions during creep age forming were conducted through experimental methods including transmission electron microscopy (TEM) study and X-ray diffraction (XRD). The obtained results were analyzed to find the general trend of microstructural evolvements.

Progress on Transonic Aircraft Flutter Prediction Methodsby Dr Nikolaos Simiriotis

sixAccurate prediction of flutter boundaries for air vehicles is crucial since flutter is a certification-critical phenomenon which ensures the safety of flight operations. Currently, flutter issues are identified only at the final design and flight-testing stages, at which point any design changes are extremely costly. Therefore, accurate and efficient flutter prediction methods can lead to significant cost savings. In the industry, the standard flutter prediction methods are based on low fidelity aerodynamics and linearized transonic equations, while in the research community the standard method is to analyze wings through costly time-accurate coupled CFD-CSD simulations. Fortunately, since flutter is a self-excited neutrally-stable periodic phenomenon, frequency-based simulations can be used to by-pass the long transient phase and accelerate the solution process. With frequency-based methods, we can represent all the state variables with a Fourier series and transform the time-dependent problem into a series of coupled steady state problems. Then, the flutter boundaries can be predicted in one-shot by searching simultaneously for the reduced velocity and the corresponding frequency. Frequency-domain methods present a lot of advantages: they are applicable to systems of generic complexity, they only seek directly the periodic solution, and they naturally introduce high-fidelity computations in the flutter prediction framework. To this end, in our presentation we discussed the direct solution methods which follow this idea, allowing to capture multiple branches of the flutter boundary accurately, whilst being approximately 30-40 times faster than the time-accurate approach.

Steering Committee Meeting - 8th January 2021

Steering Committee Meeting


COMAC (BATRI): 光辉 Prof Wuguang Hui; 叶 伟 Prof Ye Wei; 李东升 Prof Li Dongsheng; 胡震东 Prof Hu Zhendong; 张波成 Dr Zhang Bocheng; 马立敏 Dr Ma Limin; 宋清华 Dr Song Qinghua; 陈保国 Dr Chen Baoguo; Du Xi; Chen Chao; Jiajing Lyu

ICL: Prof Bamber Blackman, Prof Spencer Sherwin, Prof John Dear, Prof Jianguo Lin, Dr Zhusheng Shi, Prof Paul Robinson, Dr Francesca Pietra, Dr Jun Liu


Recent awards and promotions

The ECCOMAS Prandtl medal has recently been awarded to the Department of Aeronautics’ Professor Spencer Sherwin. Professor Sherwin, the Department’s Head of Aerodynamics, received the Medal for his outstanding and sustained contributions to computational fluid dynamics research. ECCOMAS (the European Community on Computational Methods in Applied Sciences) groups together European associations who have interests in developing and applying computational methods in science and technology. Read full story here

We are also delighted to announce a recent promotion of the Co-Director of the Imperial - COMAC Research Centre - Bamber Blackman, to the rank of Professor. Professor Blackman's research interests include the fracture mechanics of structural adhesive joints and polymeric fibre-reinforced composite materials. He is based within the Department of Mechanical Engineering. 

Networking event at Imperial College London

COMAC Networking Event

Following the Quarterly Internal Management Meeting on 21st January 2020, all investigators, researchers and PhD students currently involved in the Research Centre met for an informal networking session at the Eastside Bar on Imperial’s South Kensington Campus.

The event served as an ice breaker for everyone, aided exchange of ideas and plans for progression of individual projects. All over a well-deserved drink!

Imperial visit in Shanghai

As part of his fourteen-day trip to China, Professor Spencer Sherwin was hosted by Mr. Li Dongsheng in Shanghai on 12th December 2019.

They discussed progress of the COMAC-Imperial Research Centre over lunch.