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Anhichem, M, Timme, Sebastian ORCID: 0000-0002-2409-1686, Castagna, Jony, Peace, Andrew J and Maina, Moira
(2022)
Aerodynamic Data Modelling and Fidelity Definition for Multifidelity Data Fusion.
In: Royal Aeronautical Society Applied Aerodynamics Conference 2022.
Belesiotis-Kataras, Panagiotis and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2021)
Aeroelastic Coupling Effects in Globally Unstable Transonic Wing Flow.
In: AIAA Scitech 2021 Forum.
Anhichem, Mehdi, Timme, Sebastian ORCID: 0000-0002-2409-1686, Castagna, Jony, Peace, Andrew and Maina, Moira
(2024)
Bayesian Approaches for Efficient and Uncertainty-Aware Prediction of Pressure Distributions.
In: AIAA SCITECH 2024 Forum, 2024-1-8 - 2024-1-12, Orlanda, FL.
Vevek, US, Houtman, Jelle and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2022)
Bespoke Stability Analysis Tool in Next-Generation Computational Fluid Dynamics Solver.
In: Royal Aeronautical Society Applied Aerodynamics Conference 2022, 2022-9-13 - 2022-9-15.
Vevek, US, Houtman, Jelle and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2023)
Bespoke Stability Analysis Tool in Next-Generation Computational Fluid Dynamics Solver.
The Aeronautical Journal.
pp. 1-19.
Mykhaskiv, Orest, Mohanamuraly, Pavanakumar, Mueller, Jens-Dominik, Xu, Shenren and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2017)
CAD-based shape optimisation of the NASA CRM wing-body intersection using differentiated CAD-kernel.
In: 35th AIAA Applied Aerodynamics Conference.
Sartor, Fulvio and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2017)
Delayed Detached-Eddy Simulation of Shock Buffet on Half Wing-Body Configuration.
In: 22nd AIAA Computational Fluid Dynamics Conference, 2015-6-22 - 2015-6-26, Dallas, TX.
Pagliuca, Giampaolo and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2016)
Flight Dynamics Mode Identification and Model Reduction using Computational Fluid Dynamics.
In: AIAA Atmospheric Flight Mechanics Conference, 2016-6-13 - 2016-6-17, Washington, DC.
Timme, Sebastian ORCID: 0000-0002-2409-1686
(2019)
Global Shock Buffet Instability on NASA Common Research Model.
In: AIAA Scitech 2019 Forum, 2019-1-7 - 2019-1-11, San Diego, CA.
Timme, Sebastian ORCID: 0000-0002-2409-1686
(2018)
Global instability of wing shock buffet.
[Preprint]
Timme, Sebastian ORCID: 0000-0002-2409-1686
(2020)
Global instability of wing shock-buffet onset.
JOURNAL OF FLUID MECHANICS, 885.
Houtman, Jelle and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2023)
Global stability analysis of elastic aircraft in edge-of-the-envelope flow.
JOURNAL OF FLUID MECHANICS, 967.
Belesiotis-Kataras, Panagiotis and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2020)
Harmonic Forcing Amplitude Effects in Globally Unstable Transonic Wing Flow.
In: AIAA Scitech 2020 Forum.
Houtman, Jelle, Vevek, US and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2023)
Identifying Active Regions of Finite-Wing Transonic Buffet using Resolvent Method.
In: AIAA AVIATION 2023 Forum, 2023-6-12 - 2023-6-16.
Bekemeyer, Philipp, Thormann, Reik and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2016)
LINEARISED FREQUENCY DOMAIN GUST ANALYSIS OF LARGE CIVIL AIRCRAFT.
In: VII European Congress on Computational Methods in Applied Sciences and Engineering, 2016-6-5 - 2016-6-10, Crete Island, Greece.
Belesiotis, Panagiotis
(2022)
Methods for the Investigation of Transonic Buffet.
Doctor of Philosophy thesis, University of Liverpool.
Pagliuca, G
(2018)
Model Reduction for Flight Dynamics using Computational Fluid Dynamics.
PhD thesis, University of Liverpool.
Pagliuca, Giampaolo and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2017)
Model reduction for flight dynamics simulations using computational fluid dynamics.
AEROSPACE SCIENCE AND TECHNOLOGY, 69.
pp. 15-26.
Anhichem, Mehdi, Timme, Sebastian ORCID: 0000-0002-2409-1686, Castagna, Jony, Peace, Andrew and Maina, Moira
(2022)
Multifidelity Data Fusion Applied to Aircraft Wing Pressure Distribution.
In: AIAA AVIATION 2022 Forum, 2022-6-27 - 2022-7-1, Chicago, IL.
Gai, Guanqun and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2016)
Nonlinear reduced-order modelling for limit-cycle oscillation analysis.
Nonlinear Dynamics, 84 (2).
pp. 991-1009.
Masini, Luke ORCID: 0000-0001-5495-1627
(2021)
On Transonic Wing Shock Unsteadiness.
PhD thesis, University of Liverpool.
Thormann, Reik, Bekemeyer, Philipp and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2016)
REDUCED ORDER MODELLING OF GUST ANALYSIS USING COMPUTATIONAL FLUID DYNAMICS.
In: VII European Congress on Computational Methods in Applied Sciences and Engineering, 2016-6-5 - 2016-6-10, Crete Island, Greece.
Bekemeyer, P
(2018)
Rapid Computational Aerodynamics for Aircraft Gust Response Analysis.
PhD thesis, University of Liverpool.
Bekemeyer, Philipp and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2016)
Reduced Order Gust Response Simulation using Computational Fluid Dynamics.
In: 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2016-1-4 - 2016-1-8, San Diego, CA.
Bekemeyer, Philipp and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2017)
Reduced Order Transonic Aeroelastic Gust Response Simulation of Large Aircraft.
In: 35th AIAA Applied Aerodynamics Conference, 2017-6-5 - 2017-6-9, Denver, Colorado.
Houtman, Jelle, Timme, Sebastian ORCID: 0000-0002-2409-1686 and Sharma, Ati
(2022)
Resolvent Analysis of Large Aircraft Wings in Edge-of-the-Envelope Transonic Flow.
In: AIAA SCITECH 2022 Forum.
He, Wei ORCID: 0000-0002-2633-6114 and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2020)
Resolvent Analysis of Shock Buffet on Infinite Wings.
In: AIAA AVIATION 2020 FORUM, Virtual Event.
Vevek, US and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2023)
Resolvent Analysis using Subspace Algorithms for Aerodynamic Applications.
In: AIAA AVIATION 2023 Forum, 2023-6-12 - 2023-6-16.
Houtman, Jelle, Timme, Sebastian ORCID: 0000-0002-2409-1686 and Sharma, Ati
(2023)
Resolvent analysis of a finite wing in transonic flow.
FLOW, 3.
Masini, Luke ORCID: 0000-0001-5495-1627, Timme, Sebastian ORCID: 0000-0002-2409-1686 and Peace, Andrew J
(2019)
Reynolds Number Effects on Wing Shock Buffet Unsteadiness.
In: AIAA Aviation 2019 Forum, 2019-6-16 - 2019-6-21, Dallas, TX.
Xu, Shenren and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2017)
Robust and efficient adjoint solver for complex flow conditions.
COMPUTERS & FLUIDS, 148.
pp. 26-38.
Masini, Luke ORCID: 0000-0001-5495-1627, Timme, Sebastian ORCID: 0000-0002-2409-1686 and Peace, Andrew J
(2020)
Scale-Resolving Simulations of a Civil Aircraft Wing Transonic Shock-Buffet Experiment.
AIAA JOURNAL, 58 (10).
pp. 4322-4338.
Houtman, Jelle and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2021)
Towards Global Stability Analysis of Flexible Aircraft in Edge-of-the-Envelope Flow.
In: AIAA Scitech 2021 Forum.
Timme, Sebastian ORCID: 0000-0002-2409-1686 and Thormann, Reik
(2016)
Towards Three-Dimensional Global Stability Analysis of Transonic Shock Buffet.
In: AIAA Atmospheric Flight Mechanics Conference, 2016-6-13 - 2016-6-17, Washington, DC.
Kelly, Joshua, Fichera, Sebastiano ORCID: 0000-0003-1006-4959 and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2022)
Towards a Design Framework for High Pressure Turboexpanders.
In: ASMO-UK12 / ASMO-Europe1 / ISSMO Conference on Engineering Design Optimization, 2022-7-18 - 2022-7-19, Leeds, UK.
Moise, Pradeep, Zauner, Markus, Sandham, Neil D, Timme, Sebastian ORCID: 0000-0002-2409-1686 and He, Wei
(2023)
Transonic Buffet Characteristics Under Conditions of Free and Forced Transition.
AIAA JOURNAL, 61 (3).
pp. 1061-1076.
Timme, Sebastian
(2010)
Transonic aeroelastic instability searches using a hierarchy of aerodynamic models.
PhD thesis, University of Liverpool.
He, Wei ORCID: 0000-0002-2633-6114 and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2020)
Triglobal Shock Buffet Instability Study on Infinite Wings.
In: AIAA Scitech 2020 Forum, 2020-1-6 - 2020-1-10.
He, Wei ORCID: 0000-0002-2633-6114 and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2021)
Triglobal infinite-wing shock-buffet study.
Journal of Fluid Mechanics, 925.
Xu, Shenren, Timme, Sebastian ORCID: 0000-0002-2409-1686, Mykhaskiv, Orest and Mueller, Jens-Dominik
(2017)
Wing-body junction optimisation with CAD-based parametrisation including a moving intersection.
AEROSPACE SCIENCE AND TECHNOLOGY, 68.
pp. 543-551.