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AEROGUST
Aeroelastic Gust Modelling
Total Cost €
0EC-Contrib. €
0Partnership
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0AEROGUST project word cloud
Explore the words cloud of the AEROGUST project. It provides you a very rough idea of what is the project "AEROGUST" about.
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lattice
maximum
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methodology
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environmental
aerodynamic
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Project "AEROGUST" data sheet
The following table provides information about the project.
| Coordinator |
UNIVERSITY OF BRISTOL
Organization address contact info |
| Coordinator Country | United Kingdom [UK] |
| Project website | http://www.aerogust.eu/ |
| Total cost | 4˙289˙986 € |
| EC max contribution | 4˙237˙652 € (99%) |
| Programme |
1. H2020-EU.3.4. (SOCIETAL CHALLENGES - Smart, Green And Integrated Transport) |
| Code Call | H2020-MG-2014_TwoStages |
| Funding Scheme | RIA |
| Starting year | 2015 |
| Duration (year-month-day) | from 2015-05-01 to 2018-07-31 |
Partnership
Take a look of project's partnership.
| # | ||||
|---|---|---|---|---|
| 1 | UNIVERSITY OF BRISTOL | UK (BRISTOL) | coordinator | 827˙425.00 |
| 2 | DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV | DE (KOELN) | participant | 468˙203.00 |
| 3 | DASSAULT AVIATION | FR (PARIS) | participant | 383˙863.00 |
| 4 | THE UNIVERSITY OF LIVERPOOL | UK (LIVERPOOL) | participant | 350˙216.00 |
| 5 | NUMERICAL MECHANICS APPLICATIONS INTERNATIONAL SA | BE (BRUXELLES) | participant | 344˙625.00 |
| 6 | STICHTING NATIONAAL LUCHT- EN RUIMTEVAARTLABORATORIUM | NL (AMSTERDAM) | participant | 341˙550.00 |
| 7 | UNIVERSITY OF CAPE TOWN | ZA (RONDEBOSCH) | participant | 324˙375.00 |
| 8 | VALEOL SAS | FR (BEGLES) | participant | 318˙750.00 |
| 9 | Optimad engineering s.r.l. | IT (TORINO) | participant | 304˙250.00 |
| 10 | INSTITUT NATIONAL DE RECHERCHE ENINFORMATIQUE ET AUTOMATIQUE | FR (LE CHESNAY CEDEX) | participant | 286˙268.00 |
| 11 | PIAGGIO AERO INDUSTRIES SPA | IT (ROMA) | participant | 219˙375.00 |
| 12 | AIRBUS DEFENCE AND SPACE GMBH | DE (TAUFKIRCHEN) | participant | 68˙750.00 |
Map
Project objective
Encounters with atmospheric turbulence are a vitally important in the design and certification of many manmade structures such as aircraft and wind turbines. Gusts cause rapid changes in the flow about the structures which leads to rigid and flexible unsteady responses. Knowledge of aircraft/gust interactions is therefore vital for loads estimation during aircraft design as it impacts on control systems and often defines the maximum loads that these structures will experience in service. At present industry typically uses the linear doublet lattice method with static loads corrections from expensive wind tunnel data. The wind tunnel data is created using the final aerodynamic surface in the predicted cruise shape. This means that gust loads come relatively late when the design options have been narrowed. Increased competition and environmental concerns are likely to lead to the adoption of more flexible materials and the consideration of novel configurations, in which case the linear assumptions of the current gust loads process will become unacceptable. To introduce non-linearity into the gust loads process without significantly increasing the cost and time, this project has three main objectives: to carry out investigations using CFD so that the non-linearities in gust interactions are understood; to create a gust loads process that does not require wind tunnel data and hence reduces the need for wind tunnel testing; to develop updated reduced order models for gust prediction that account for non-linearity at an acceptable cost. These investigations will reduce the need for expensive wind tunnel testing and hence lead to time and cost savings at the design stage therefore ensuring that the European aerospace and defence industry remain competitive in the future. The wind turbine industry has similar concerns, with gusts and wind shear restricting the locations available for wind farms. The project will also address these issues using common methodology.
Deliverables
| Final report: Analysis of the AEROGUST project results: impact on gust response prediction. | Documents, reports | 2019-06-07 18:02:26 |
| Report on the decoupling of aeroelastic corrections and the gust model. | Documents, reports | 2019-06-07 18:02:25 |
| Preliminary exploitation report for milestone review | Documents, reports | 2019-06-07 18:02:24 |
| Report on Fourier Decomposition ROM for gusts. | Documents, reports | 2019-06-07 18:02:25 |
| Report on coupling of reduced order aerodynamic model with full order finite element structural models. | Documents, reports | 2019-06-07 18:02:25 |
| Final report on Dissemination and Exploitation | Documents, reports | 2019-06-07 18:02:24 |
| Report on the impact of linear history effects on the aeroelastic model and gust. | Documents, reports | 2019-06-07 18:02:25 |
| Report on application of hybrid methods to investigate feasibility for possible future full aircraft gust simulations. | Documents, reports | 2019-06-07 18:02:25 |
| Final report of WP4. | Documents, reports | 2019-06-07 18:02:25 |
| Final report on ROMs created directly from virtual experiment. | Documents, reports | 2019-06-07 18:02:25 |
| Report on comparison between free air results and results from industrial gust loads process. | Documents, reports | 2019-06-07 18:02:25 |
| Report on updating nonlinear state space aerodynamic ROMs. | Documents, reports | 2019-06-07 18:02:25 |
| Report on simultaneous gust and control surface deflection | Documents, reports | 2019-06-07 18:02:26 |
| Report on simulations of coupled non-linear aerodynamics with full order geometrically non-linear finite-element structural models | Documents, reports | 2019-06-07 18:02:25 |
| Final report on projection ROM. | Documents, reports | 2019-06-07 18:02:25 |
| Report on the effects of uncertainty on the gust loads process | Documents, reports | 2019-06-07 18:02:25 |
| Report on hybrid outer ROM and inner higher fidelity method. | Documents, reports | 2019-06-07 18:02:25 |
| Final Report of WP3. | Documents, reports | 2019-06-07 18:02:24 |
| Report on extension of the developed methods to wind turbine applications. | Documents, reports | 2019-06-07 18:02:26 |
| Report on analysis of the impact of gust definitions for coupled 6-DoF rigid model aircraft compared to the new gust definitions. | Documents, reports | 2019-06-07 18:02:24 |
| Report on methods for introducing non-linear history effects in the gust analysis via CFD. | Documents, reports | 2019-06-07 18:02:26 |
| Report on the investigation of predicted non-linear behaviour using a high order hybrid zonal method for the simulation of the aircraft/gust interaction. | Documents, reports | 2019-06-07 18:02:24 |
| Report on aerodynamic reduced order models updated using high fidelity numerical free air data. | Documents, reports | 2019-06-07 18:02:26 |
| Report on updating aerodynamic ROMs via constraints. | Documents, reports | 2019-06-07 18:02:26 |
| Report on coupling reduced order aerodynamic model with reduced order structural models. | Documents, reports | 2019-06-07 18:02:25 |
| Final report of WP2 which evaluates the effects of non-linearities on gusts load prediction. | Documents, reports | 2019-06-07 18:02:25 |
| Final report on the prediction of non-linear behaviour using Boundary Condition Methods. | Documents, reports | 2019-06-07 18:02:25 |
| Second year report on comparison and evaluation of results. | Documents, reports | 2019-06-07 18:02:25 |
| Report on methods developed for determining effects of uncertainties on Continuous Turbulence gust loads. | Documents, reports | 2019-06-07 18:02:25 |
| Report on using multiple flight shape models for aeroelastic corrections. | Documents, reports | 2019-06-07 18:02:25 |
| Final project booklet of results | Documents, reports | 2019-06-07 18:02:24 |
| Report on the application of LES/DES Methods to aerofoil geometries. | Documents, reports | 2019-06-07 18:02:24 |
| Final report on collection of in-service wind turbine data. | Documents, reports | 2019-06-07 18:02:25 |
| Final report on integration of zonal POD/CFD methods with structural models. | Documents, reports | 2019-06-07 18:02:26 |
| Report on aeroelastic ROMs for wind turbines using CFD and in-service data. | Documents, reports | 2019-06-07 18:02:25 |
| Report on methods developed for determining effects of uncertainties on worst case “1-cosine†gust loads. | Documents, reports | 2019-06-07 18:02:24 |
| Report on aeroelastic Fourier decomposition ROM for gusts. | Documents, reports | 2019-06-07 18:02:25 |
| Report on comparison of gust ROMs with gusts computed with Linear Frequency Domain solver and TAU. | Documents, reports | 2019-06-07 18:02:25 |
| Interim report on projection ROM. | Documents, reports | 2019-06-07 18:02:24 |
| Initial report on the prediction of non-linear behaviour using Boundary Condition Methods. | Documents, reports | 2019-06-07 18:02:23 |
| Report on the prediction of non-linear behaviour using Field and Split Velocity Methods. | Documents, reports | 2019-06-07 18:02:23 |
| Report on the investigation of Atmospheric Disturbance for Aircraft Gust Loads Application. | Documents, reports | 2019-06-07 18:02:23 |
| Initial report on projection ROM. | Documents, reports | 2019-06-07 18:02:24 |
| Public web site and LinkedIn profile set up for AEROGUST. | Websites, patent fillings, videos etc. | 2019-06-07 18:02:24 |
| Report on analysis of the non-linear behaviour using bifurcation theory applied to the coupled aeroelastic system with an assumed mode model of the non-linear structure. | Documents, reports | 2019-06-07 18:02:24 |
| Methodology for validation, accuracy estimation and model comparison. | Documents, reports | 2019-06-07 18:02:24 |
| Final report on recreating the current industrial loads process. | Documents, reports | 2019-06-07 18:02:24 |
| Interim report on ROMs created directly from virtual experiment. | Documents, reports | 2019-06-07 18:02:24 |
| Report on coupling with full order geometrically non-linear finite-element structural models | Documents, reports | 2019-06-07 18:02:24 |
| Report identifying common cases geometries and test cases. | Documents, reports | 2019-06-07 18:02:24 |
| Working Solution Data Base. | Websites, patent fillings, videos etc. | 2019-06-07 18:02:24 |
| Report on the Solution Data Base giving justifications and templates for users. | Documents, reports | 2019-06-07 18:02:24 |
| Report on investigation of predicted non-linear behaviour of wind-turbine blades gust behaviour. | Documents, reports | 2019-06-07 18:02:24 |
| Project leaflet to identified stakeholders | Websites, patent fillings, videos etc. | 2019-06-07 18:02:24 |
| Report on dissemination strategy | Documents, reports | 2019-06-07 18:02:24 |
| Initial report identifying common cases geometries and test cases. | Documents, reports | 2019-06-07 18:02:24 |
| First year report on comparison and evaluation of results. | Documents, reports | 2019-06-07 18:02:24 |
| Initial report on recreating the current industrial loads process. | Documents, reports | 2019-06-07 18:02:24 |
| Report reviewing test cases and identifying any modifications as a result of year 1 work. | Documents, reports | 2019-06-07 18:02:24 |
| AEROGUST Project Presentation | Documents, reports | 2019-06-07 18:02:24 |
| Survey and Characterisation of High Fidelity LES/DES Methods for Gust Simulation. | Documents, reports | 2019-06-07 18:02:23 |
Take a look to the deliverables list in detail: detailed list of AEROGUST deliverables.
Publications
| year | authors and title | journal | last update |
|---|---|---|---|
| 2017 |
Wales, C., Cook, R. G., Jones, D. P. & Gaitonde, A. L. Comparison of Aerodynamic Models for 1-Cosine Gust Loads Prediction published pages: , ISSN: , DOI: |
International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017): 25-28 June 2017, Como - Italy. | 2019-06-07 |
| 2018 |
Michel Bergmann, Andrea Ferrero, Angelo Iollo, Edoardo Lombardi, Angela Scardigli, Haysam Telib A zonal Galerkin-free POD model for incompressible flows published pages: 301-325, ISSN: 0021-9991, DOI: 10.1016/j.jcp.2017.10.001 |
Journal of Computational Physics 352 | 2019-06-07 |
| 2017 |
Ralf Heinrich, Lars Reimer Comparison of different approaches for modeling of atmospheric effects like gusts and wake-vortices in the CFD Code TAU published pages: , ISSN: , DOI: |
International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017) | 2019-06-07 |
| 2016 |
Bergmann, Michel;Â Ferrero, Andrea;Â Iollo, Angelo;Â Scardigli, A;Â Telib, Haysam An approach to perform shape optimisation by means of hybrid ROM-CFD simulations published pages: , ISSN: , DOI: |
Institut Henri Poincaré Conference: Recent developments in numerical methods for model reduction | 2019-06-07 |
| 2017 |
R. Thormann, S. Timme Efficient aerodynamic derivative calculation in three-dimensional transonic flow published pages: 1464-1478, ISSN: 0001-9240, DOI: 10.1017/aer.2017.66 |
The Aeronautical Journal 121/1244 | 2019-06-07 |
| 2017 |
Simeone, S., Rendall, T., Williams, S., Wales, C., Cooper, J., Jones, D. & Gaitonde, A. Reconstruction of Gust Velocity Profiles via Potential Flow, CFD and ROM Techniques published pages: , ISSN: , DOI: |
International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017): 25-28 June 2017, Como - Italy. | 2019-06-07 |
| 2017 |
W.Man, A.B.Mowat, A.G.Malan and J.Farao A CFD Based Aeroelastic Gust model for Full Aircraft Simulation published pages: , ISSN: , DOI: |
International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017) | 2019-06-07 |
| 2017 |
Kaiser, Christoph and Friedewald, Diliana and Nitzsche, Jens Comparison of Nonlinear CFD with Time-Linearized CFD and CFD-Corrected DLM for Gust Encounter Simulations published pages: , ISSN: , DOI: |
International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017) | 2019-06-07 |
| 2017 |
Stefan Görtz, Matteo Ripepi Towards Reduced Order Modeling for Gust Simulations published pages: , ISSN: , DOI: |
Conference: Deutscher Luft- und Raumfahrtkongress (DLRK) 2017 | 2019-06-07 |
| 2017 |
J.C.Farao, A.G.Malan and F.Gambioli Towards a Non-linear Full Aircraft Model for Passenger Aircraft Loads Calculations published pages: , ISSN: , DOI: |
International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017) | 2019-06-07 |
| 2018 |
Dorian Jones, Ann Gaitonde The AeroGust Project published pages: , ISSN: , DOI: |
Royal Aeronautical Society Future of Aerodynamics Conference 2018 | 2019-06-07 |
| 2016 |
Michel Bergmann, Andrea Ferrero, Angelo Iollo A POD model for boundary conditions in CFD published pages: , ISSN: , DOI: |
Ninth International Conference on Computational Fluid Dynamics (ICCFD9) | 2019-06-07 |
| 2017 |
Angelo Iollo, Michel Bergmann, Andrea Ferrero, Haysam Telib A reduced-order model for NS equations from boundary matching and OT published pages: , ISSN: , DOI: |
SIAM Conference on Computational Science and Engineering | 2019-06-07 |
| 2017 |
Cook, R., Wales, C. J. A., Gaitonde, A. L., Jones, D. P. & Cooper, J. E. Uncertainty Quantification in Gust Loads Analysis of a Highly Flexible Aircraft Wing published pages: , ISSN: , DOI: |
International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017) | 2019-06-07 |
| 2018 |
Tomas Lundquist, Arnaud Malan, Jan Nordström A hybrid framework for coupling arbitrary summation-by-parts schemes on general meshes published pages: 49-68, ISSN: 0021-9991, DOI: 10.1016/j.jcp.2018.02.018 |
Journal of Computational Physics 362 | 2019-06-07 |
| 2017 |
Reik Thormann, Sebastian Timme, G Pagliuca Influence of Gust Modelling on Free-Flight Aerofoils published pages: , ISSN: , DOI: |
International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017) | 2019-06-07 |
| 2017 |
D. M. Changfoot, W. Liu Tat Man, R. A. D. Horwitz, A. G. B. Mowat, J. C. Farao, A. G. Malan Toward Improved Non-linear Aeroelastic Modelling For Design published pages: , ISSN: , DOI: |
Zienkiewicz Centre for Computational Engineering seminar series | 2019-06-07 |
| 2016 |
Bergmann, Michel; Ferrero, Andrea A hybrid DNS-ROM approach for gust computations published pages: , ISSN: , DOI: |
The 7th International Conference on Computational Methods, ICCM2016 | 2019-06-07 |
| 2015 |
Robert Cook (University of Bristol) and Chris Wales (University of Bristol) AEROGUST Project presentation published pages: , ISSN: , DOI: |
The Airbus Flight Physics Distributed Partnership R&T - DiPaRT 2015 - oral presentation | 2019-06-07 |
| 2016 |
M. Ripepi (1), R. Zimmermann (2) and S. Görtz (1)
(1) German Aerospace Center (DLR)
(2) Institute Computational Mathematics, TU Braunschweig, Germany Minimum residual based model order reduction approach for unsteady nonlinear aerodynamic problems published pages: , ISSN: , DOI: |
Workshop on Data-Driven Model Order Reduction and Machine Learning (MORML 2016) - oral presentation | 2019-06-07 |
| 2016 |
M. Ripepi, N. Karcher, T. Franz, M. Abu-Zurayk, and S. Görtz (German Aerospace Center - DLR) CFD-based ROMs for Aeronautical Applications published pages: , ISSN: , DOI: |
COST EU-MORNET WG1 mini-workshop: ROM for CFD - oral presentation | 2019-06-07 |
| 2015 |
All partners in the Aerogust project AEROGUST Project presentation published pages: , ISSN: , DOI: |
2019-06-07 | |
| 2016 |
Ferrero, Andrea; Bergmann, Michel; Iollo, Angelo Different approaches to the development of reduced-order models for NS equations published pages: , ISSN: , DOI: |
ALOP Workshop: Reduced Order Models in Optimization - oral presentation | 2019-06-07 |
| 2016 |
A. Gaitonde, D. Jones and J. E. Cooper (University of Bristol) AEROGUST Project overview article published pages: Page 48, ISSN: , DOI: |
EU Research Magazine | 2019-06-07 |
| 2017 |
Angelo Iollo, Michel Bergmann, Andrea Ferrero, Haysam Telib Advection Modes and Model Reduction by Proper Orthogonal Decompostion published pages: , ISSN: , DOI: |
Conference on Classical and Geophysical Fluid Dynamics Modeling, Reduction and Simulation | 2019-06-07 |
| 2017 |
S. Görtz, M. Ripepi , T Franz, M Abu-Zurayk, R. , Zimmermann Reduced order models for aerodynamic applications, loads and MDO published pages: , ISSN: , DOI: |
3rd Workshop on Model Reduction of Complex Dynamical Systems (MODRED 2017)Â | 2019-06-07 |
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