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Aeroelastic Gust Modelling

Livrables

Final report on Dissemination and Exploitation

Final report on Dissemination and Exploitation

Report on the decoupling of aeroelastic corrections and the gust model.

Report on the decoupling of aeroelastic corrections and the gust model.

Report on aeroelastic ROMs for wind turbines using CFD and in-service data.

Report on aeroelastic ROMs for wind turbines using CFD and in-service data.

AEROGUST Project Presentation

AEROGUST Project Presentation

Final report on the prediction of non-linear behaviour using Boundary Condition Methods.

Final report on the prediction of non-linear behaviour using Boundary Condition Methods.

Report on coupling of reduced order aerodynamic model with full order finite element structural models.

Report on coupling of reduced order aerodynamic model with full order finite element structural models.

Report on methods developed for determining effects of uncertainties on Continuous Turbulence gust loads.

Report on methods developed for determining effects of uncertainties on Continuous Turbulence gust loads.

Final report: Analysis of the AEROGUST project results: impact on gust response prediction.

Final report: Analysis of the AEROGUST project results: impact on gust response prediction.

Final Report of WP3.

Final Report of WP3.

First year report on comparison and evaluation of results.

First year report on comparison and evaluation of results.

Report reviewing test cases and identifying any modifications as a result of year 1 work.

Report reviewing test cases and identifying any modifications as a result of year 1 work

Report on hybrid outer ROM and inner higher fidelity method.

Report on hybrid outer ROM and inner higher fidelity method.

Initial report on projection ROM.

Initial report on projection ROM.

Second year report on comparison and evaluation of results.

Second year report on comparison and evaluation of results.

Report on aerodynamic reduced order models updated using high fidelity numerical free air data.

Report on aerodynamic reduced order models updated using high fidelity numerical free air data.

Report on analysis of the impact of gust definitions for coupled 6-DoF rigid model aircraft compared to the new gust definitions.

Report on analysis of the impact of gust definitions for coupled 6-DoF rigid model aircraft compared to the new gust definitions.

Preliminary exploitation report for milestone review

Preliminary exploitation report for milestone review

Final report on ROMs created directly from virtual experiment.

Final report on ROMs created directly from virtual experiment.

Interim report on ROMs created directly from virtual experiment.

Interim report on ROMs created directly from virtual experiment.

Final project booklet of results

Final project booklet of results

Report on aeroelastic Fourier decomposition ROM for gusts.

Report on aeroelastic Fourier decomposition ROM for gusts.

Report on extension of the developed methods to wind turbine applications.

Report on extension of the developed methods to wind turbine applications.

Interim report on projection ROM.

Interim report on projection ROM.

Report on updating aerodynamic ROMs via constraints.

Report on updating aerodynamic ROMs via constraints.

Report on simulations of coupled non-linear aerodynamics with full order geometrically non-linear finite-element structural models

Report on simulations of coupled non-linear aerodynamics with full order geometrically non-linear finite-element structural models

Report on coupling with full order geometrically non-linear finite-element structural models

Report on coupling with full order geometrically non-linear finite-element structural models

Report on the investigation of Atmospheric Disturbance for Aircraft Gust Loads Application.

Report on the investigation of Atmospheric Disturbance for Aircraft Gust Loads Application

Final report on integration of zonal POD/CFD methods with structural models.

Final report on integration of zonal POD/CFD methods with structural models.

Initial report on the prediction of non-linear behaviour using Boundary Condition Methods.

Initial report on the prediction of nonlinear behaviour using Boundary Condition Methods

Report on the Solution Data Base giving justifications and templates for users.

Report on the Solution Data Base giving justifications and templates for users

Methodology for validation, accuracy estimation and model comparison.

Methodology for validation accuracy estimation and model comparison

Report on investigation of predicted non-linear behaviour of wind-turbine blades gust behaviour.

Report on investigation of predicted non-linear behaviour of wind-turbine blades gust behaviour.

Final report on recreating the current industrial loads process.

Final report on recreating the current industrial loads process

Report on application of hybrid methods to investigate feasibility for possible future full aircraft gust simulations.

Report on application of hybrid methods to investigate feasibility for possible future full aircraft gust simulations.

Report on the impact of linear history effects on the aeroelastic model and gust.

Report on the impact of linear history effects on the aeroelastic model and gust.

Final report on collection of in-service wind turbine data.

Final report on collection of in-service wind turbine data.

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.

Report on analysis of the nonlinear behaviour using bifurcation theory applied to the coupled aeroelastic system with an assumed mode model of the nonlinear structure

Report identifying common cases geometries and test cases.

Report identifying common cases geometries and test cases

Report on comparison between free air results and results from industrial gust loads process.

Report on comparison between free air results and results from industrial gust loads process.

Report on comparison of gust ROMs with gusts computed with Linear Frequency Domain solver and TAU.

Report on comparison of gust ROMs with gusts computed with Linear Frequency Domain solver and TAU.

Report on the application of LES/DES Methods to aerofoil geometries.

Report on the application of LES/DES Methods to aerofoil geometries.

Report on the effects of uncertainty on the gust loads process

Report on the effects of uncertainty on the gust loads process

Report on methods developed for determining effects of uncertainties on worst case “1-cosine” gust loads.

Report on methods developed for determining effects of uncertainties on worst case “1-cosine” gust loads.

Final report of WP4.

Final report of WP4.

Final report of WP2 which evaluates the effects of non-linearities on gusts load prediction.

Final report of WP2 which evaluates the effects of non-linearities on gusts load prediction.

Report on the prediction of non-linear behaviour using Field and Split Velocity Methods.

Report on the prediction of nonlinear behaviour using Field and Split Velocity Methods

Initial report identifying common cases geometries and test cases.

Initial report identifying common cases geometries and test cases

Report on methods for introducing non-linear history effects in the gust analysis via CFD.

Report on methods for introducing non-linear history effects in the gust analysis via CFD.

Report on coupling reduced order aerodynamic model with reduced order structural models.

Report on coupling reduced order aerodynamic model with reduced order structural models.

Initial report on recreating the current industrial loads process.

Initial report on recreating the current industrial loads process.

Report on using multiple flight shape models for aeroelastic corrections.

Report on using multiple flight shape models for aeroelastic corrections.

Survey and Characterisation of High Fidelity LES/DES Methods for Gust Simulation.

Survey and Characterisation of High Fidelity LESDES Methods for Gust Simulation

Report on Fourier Decomposition ROM for gusts.

Report on Fourier Decomposition ROM for gusts.

Report on the investigation of predicted non-linear behaviour using a high order hybrid zonal method for the simulation of the aircraft/gust interaction.

Report on the investigation of predicted non-linear behaviour using a high order hybrid zonal method for the simulation of the aircraft/gust interaction.

Report on simultaneous gust and control surface deflection

Report on simultaneous gust and control surface deflection

Report on dissemination strategy

Report on dissemination strategy

Final report on projection ROM.

Final report on projection ROM.

Report on updating nonlinear state space aerodynamic ROMs.

Report on updating nonlinear state space aerodynamic ROMs.

Working Solution Data Base.

Working Solution Data Base

Public web site and LinkedIn profile set up for AEROGUST.

Public web site and LinkedIn profile set up for AEROGUST.

Project leaflet to identified stakeholders

Project leaflet to identified stakeholders

Recherche de données OpenAIRE...

Publications

Efficient Modelling of a Nonlinear Gust Loads Process for Uncertainty Quantification of Highly Flexible Aircraft

Auteurs: Robert G. Cook, Christopher Wales, Ann Gaitonde, Dorian Jones, Jonathan E. Cooper
Publié dans: 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018, ISBN 978-1-62410-532-6
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-1681

Worst Case Gust Prediction of Highly Flexible Wings

Auteurs: Robbie Cook, Dario Calderon, Mark H. Lowenberg, Simon Nield, Jonathan E. Cooper, Etienne Coetzee
Publié dans: 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2017, ISBN 978-1-62410-453-4
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2017-1355

Application of Harmonic Balance Method for Non-linear Gust Responses

Auteurs: Reik Thormann, Sebastian Timme
Publié dans: 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018, ISBN 978-1-62410-532-6
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-1686

Comparison of Aerodynamic Models for 1-Cosine Gust Loads Prediction

Auteurs: Wales, C., Cook, R. G., Jones, D. P. & Gaitonde, A. L.
Publié dans: International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017): 25-28 June 2017, Como - Italy., 2017
Éditeur: International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017): 25-28 June 2017, Como - Italy.

Reconstruction of Gust Velocity Profiles via Potential Flow, CFD and ROM Techniques

Auteurs: Simeone, S., Rendall, T., Williams, S., Wales, C., Cooper, J., Jones, D. & Gaitonde, A.
Publié dans: International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017): 25-28 June 2017, Como - Italy., 2017
Éditeur: International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017): 25-28 June 2017, Como - Italy.

The Future of Non-linear Modelling of Aeroelastic Gust Interaction

Auteurs: Christopher Wales, Carmine Valente, Robert Cook, Ann Gaitonde, Dorian Jones, Jonathan E. Cooper
Publié dans: 2018 Applied Aerodynamics Conference, 2018, ISBN 978-1-62410-559-3
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3632

A Kriging Based Corrected Potential Flow ROM for Gust Load Calculations

Auteurs: Arnaud G. Malan
Publié dans: 2018 Applied Aerodynamics Conference, 2018, ISBN 978-1-62410-559-3
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3633

High Fidelity Gust Simulations Over a Supercritical Airfoil

Auteurs: Benoit Tartinville, Virginie Barbieux, Lionel Temmerman
Publié dans: 2018 Applied Aerodynamics Conference, 2018, ISBN 978-1-62410-559-3
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3634

Nonlinear Unsteady Reduced Order Models based on Computational Fluid Dynamics for Gust Loads Predictions

Auteurs: Philipp Bekemeyer, Matteo Ripepi, Ralf Heinrich, Stefan Goertz
Publié dans: 2018 Applied Aerodynamics Conference, 2018, ISBN 978-1-62410-559-3
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3635

Uncertainty Quantification of Aeroelastic Systems with Structural or Aerodynamic Nonlinearities

Auteurs: Robert G. Cook, Christopher Wales, Ann Gaitonde, Dorian Jones, Jonathan E. Cooper, Benoit Tartinville, Harmen van der Ven
Publié dans: 2018 Applied Aerodynamics Conference, 2018, ISBN 978-1-62410-559-3
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3636

Uncertainty Quantification in Gust Loads Analysis of a Highly Flexible Aircraft Wing

Auteurs: Cook, R., Wales, C. J. A., Gaitonde, A. L., Jones, D. P. & Cooper, J. E.
Publié dans: International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017), 2017
Éditeur: International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017)

Influence of Gust Modelling on Free-Flight Aerofoils

Auteurs: Reik Thormann, Sebastian Timme, G Pagliuca
Publié dans: International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017), 2017
Éditeur: International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017)

Comparison of different approaches for modeling of atmospheric effects like gusts and wake-vortices in the CFD Code TAU

Auteurs: Ralf Heinrich, Lars Reimer
Publié dans: International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017), 2017
Éditeur: International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017)

Towards a Non-linear Full Aircraft Model for Passenger Aircraft Loads Calculations

Auteurs: J.C.Farao, A.G.Malan and F.Gambioli
Publié dans: International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017), 2017
Éditeur: International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017)

A CFD Based Aeroelastic Gust model for Full Aircraft Simulation

Auteurs: W.Man, A.B.Mowat, A.G.Malan and J.Farao
Publié dans: International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017), 2017
Éditeur: International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017)

Towards Reduced Order Modeling for Gust Simulations

Auteurs: Stefan Görtz, Matteo Ripepi
Publié dans: Conference: Deutscher Luft- und Raumfahrtkongress (DLRK) 2017, 2017
Éditeur: Conference: Deutscher Luft- und Raumfahrtkongress (DLRK) 2017

A POD model for boundary conditions in CFD

Auteurs: Michel Bergmann, Andrea Ferrero, Angelo Iollo
Publié dans: Ninth International Conference on Computational Fluid Dynamics (ICCFD9), 2016
Éditeur: Ninth International Conference on Computational Fluid Dynamics (ICCFD9)

An approach to perform shape optimisation by means of hybrid ROM-CFD simulations

Auteurs: Bergmann, Michel; Ferrero, Andrea; Iollo, Angelo; Scardigli, A; Telib, Haysam
Publié dans: Institut Henri Poincaré Conference: Recent developments in numerical methods for model reduction, 2016
Éditeur: Institut Henri Poincaré Conference: Recent developments in numerical methods for model reduction

Reduced order models for aerodynamic applications, loads and MDO

Auteurs: S. Görtz, M. Ripepi , T Franz, M Abu-Zurayk, R. , Zimmermann
Publié dans: 3rd Workshop on Model Reduction of Complex Dynamical Systems (MODRED 2017) , 2017
Éditeur: 3rd Workshop on Model Reduction of Complex Dynamical Systems (MODRED 2017) 

A reduced-order model for NS equations from boundary matching and OT

Auteurs: Angelo Iollo, Michel Bergmann, Andrea Ferrero, Haysam Telib
Publié dans: SIAM Conference on Computational Science and Engineering, 2017
Éditeur: SIAM Conference on Computational Science and Engineering

Advection Modes and Model Reduction by Proper Orthogonal Decompostion

Auteurs: Angelo Iollo, Michel Bergmann, Andrea Ferrero, Haysam Telib
Publié dans: Conference on Classical and Geophysical Fluid Dynamics Modeling, Reduction and Simulation, 2017
Éditeur: Conference on Classical and Geophysical Fluid Dynamics Modeling, Reduction and Simulation

Toward Improved Non-linear Aeroelastic Modelling For Design

Auteurs: D. M. Changfoot, W. Liu Tat Man, R. A. D. Horwitz, A. G. B. Mowat, J. C. Farao, A. G. Malan
Publié dans: Zienkiewicz Centre for Computational Engineering seminar series, 2017
Éditeur: University of Swansea

Efficient Aerodynamic Derivative Calculation in Three-Dimensional Transonic Flow

Auteurs: Reik Thormann, Sebastian Timme
Publié dans: Royal Aeronautical Society Future of Aerodynamics Conference 2016, 2016
Éditeur: Royal Aeronautical Society

Comparison of Nonlinear CFD with Time-Linearized CFD and CFD-Corrected DLM for Gust Encounter Simulations

Auteurs: Kaiser, Christoph and Friedewald, Diliana and Nitzsche, Jens
Publié dans: International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017), 2017
Éditeur: International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017)

The AeroGust Project

Auteurs: Dorian Jones, Ann Gaitonde
Publié dans: Royal Aeronautical Society Future of Aerodynamics Conference 2018, 2018
Éditeur: aerogust.eu

REDUCED ORDER MODELLING OF GUST ANALYSIS USING COMPUTATIONAL FLUID DYNAMICS

Auteurs: Reik Thormann, Philipp Bekemeyer, Sebastian Timme
Publié dans: Proceedings of the VII European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS Congress 2016), 2016, Page(s) 7423-7434, ISBN 978-618-82844-0-1
Éditeur: Institute of Structural Analysis and Antiseismic Research School of Civil Engineering National Technical University of Athens (NTUA) Greece
DOI: 10.7712/100016.2343.5441

An approach to predict gust effects by means of hybrid ROM/CFD simulations

Auteurs: Ferrero, Andrea; Telib, H; Iollo, Angelo; Bergmann, Michel
Publié dans: ECCOMAS Congress 2016 Proceedings, 2016, ISBN 978-618-82844-0-1
Éditeur: Institute of Structural Analysis and Antiseismic Research School of Civil Engineering and National Technical University of Athens (NTUA) Greece

CFD-based ROMs for Aeronautical Applications

Auteurs: M. Ripepi, N. Karcher, T. Franz, M. Abu-Zurayk, and S. Görtz (German Aerospace Center - DLR)
Publié dans: COST EU-MORNET WG1 mini-workshop: ROM for CFD - oral presentation, 2016
Éditeur: DLR

Different approaches to the development of reduced-order models for NS equations

Auteurs: Ferrero, Andrea; Bergmann, Michel; Iollo, Angelo
Publié dans: ALOP Workshop: Reduced Order Models in Optimization - oral presentation, 2016
Éditeur: INRIA

Minimum residual based model order reduction approach for unsteady nonlinear aerodynamic problems

Auteurs: M. Ripepi (1), R. Zimmermann (2) and S. Görtz (1) (1) German Aerospace Center (DLR) (2) Institute Computational Mathematics, TU Braunschweig, Germany
Publié dans: Workshop on Data-Driven Model Order Reduction and Machine Learning (MORML 2016) - oral presentation, 2016
Éditeur: DLR

A hybrid DNS-ROM approach for gust computations

Auteurs: Bergmann, Michel; Ferrero, Andrea
Publié dans: The 7th International Conference on Computational Methods, ICCM2016, 2016
Éditeur: Scientech Publisher llc, USA, 2016

A hybrid framework for coupling arbitrary summation-by-parts schemes on general meshes

Auteurs: Tomas Lundquist, Arnaud Malan, Jan Nordström
Publié dans: Journal of Computational Physics, 362, 2018, Page(s) 49-68, ISSN 0021-9991
Éditeur: Academic Press
DOI: 10.1016/j.jcp.2018.02.018

A zonal Galerkin-free POD model for incompressible flows

Auteurs: Michel Bergmann, Andrea Ferrero, Angelo Iollo, Edoardo Lombardi, Angela Scardigli, Haysam Telib
Publié dans: Journal of Computational Physics, 352, 2018, Page(s) 301-325, ISSN 0021-9991
Éditeur: Academic Press
DOI: 10.1016/j.jcp.2017.10.001

Efficient aerodynamic derivative calculation in three-dimensional transonic flow

Auteurs: R. Thormann, S. Timme
Publié dans: The Aeronautical Journal, 121/1244, 2017, Page(s) 1464-1478, ISSN 0001-9240
Éditeur: Royal Aeronautical Society
DOI: 10.1017/aer.2017.66

AEROGUST Project presentation

Auteurs: All partners in the Aerogust project
Publié dans: 2015
Éditeur: University of Bristol

AEROGUST Project overview article

Auteurs: A. Gaitonde, D. Jones and J. E. Cooper (University of Bristol)
Publié dans: EU Research Magazine, 2016, Page(s) Page 48
Éditeur: Blazon Publishing and Media Ltd

AEROGUST Project presentation

Auteurs: Robert Cook (University of Bristol) and Chris Wales (University of Bristol)
Publié dans: The Airbus Flight Physics Distributed Partnership R&T - DiPaRT 2015 - oral presentation, 2015
Éditeur: University of Bristol