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Ata Onur Başkaya
Ata Onur Başkaya
Aerodynamics Group, Faculty of Aerospace Engineering, TU Delft
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Verification and validation of immersed boundary solvers for hypersonic flows with gas-surface interactions
AO Başkaya, M Capriati, D Ninni, F Bonelli, G Pascazio, A Turchi, T Magin, ...
AIAA Aviation 2022 Forum, 3276, 2022
162022
Assessment of immersed boundary methods for hypersonic flows with gas–surface interactions
AO Başkaya, M Capriati, A Turchi, T Magin, S Hickel
Computers & Fluids 270, 106134, 2024
52024
CFD Analysis of the Cork-Phenolic Heat Shield of a Reentry Cubesat in Arc-Jet Conditions Including Ablation and Pyrolysis
AO Başkaya, A Turchi, G Bellas-Chatzigeorgis, T Magin, P Barbante
15th International Planetary Probe Workshop, 2018
32018
A conservative cut-cell immersed boundary method for accurate simulation of hypersonic flows with gas-surface interactions
AO Başkaya, S Hickel
57th 3AF international conference on applied aerodynamics, 2023
22023
An Accurate Reconstruction and Interpolation Scheme for a Conservative Cut-Cell Immersed Boundary Method with Gas-Surface Interactions
AO Başkaya, S Hickel
1*
Influence of Ablation on Laminar-Turbulent Transition over Compression Ramp at Mach 8
A Baskaya, S Hickel
12th International Conference on Computational Fluid Dynamics, 2024
2024
Fluid Ablation Interactions on a Compression Ramp at Mach 8
AO Başkaya, SD Dungan, S Hickel, C Brehm
American Institute of Aeronautics and Astronautics, 2024
2024
A Conservative Cut-Cell Immersed Boundary Solver for Accurate Simulation of Hypersonic Flows with Gas-Surface Interactions
AO Başkaya, S Hickel
2nd International Conference on Flight Vehicles, Aerothermodynamics and Re …, 2022
2022
Coupling of an Immersed Boundary Finite Volume Solver with an Aerothermodynamic Library for Atmospheric Entry Applications
AO Başkaya
2020
Coupling of an Immersed Boundary Finite Volume Solver with an Aerothermodynamic Library for Atmospheric Entry Applications MSc Thesis
AO Başkaya
El sistema no puede realizar la operación en estos momentos. Inténtalo de nuevo más tarde.
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