Data

AVT-352 Hypersonic RANS Dataset - Eilmer

The University of Queensland
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ctx_ver=Z39.88-2004&rft_val_fmt=info%3Aofi%2Ffmt%3Akev%3Amtx%3Adc&rfr_id=info%3Asid%2FANDS&rft_id=https://espace.library.uq.edu.au/view/UQ:dca5330&rft.title=AVT-352 Hypersonic RANS Dataset - Eilmer&rft.publisher=The University of Queensland&rft.description=As part of NATO Advanced Vehicle Technology working group 352, Eilmer has been used to simulate a set of double cone experiments, to be compared with other codes and with experimental data from CUBRC.This dataset contains the entire set of Eilmer calculations run for AVT-352, including input files, grid generation scripts, log files, and converged flow field data. Post processing scripts are also provided, which are written in the python programming language.The github page linked above contains heat transfer and wall pressure predictions for all of the codes involved with AVT-352, Eilmer included.&rft.creator=Anonymous&rft.date=2024&rft_rights=2024, The University of Queensland&rft_rights= https://guides.library.uq.edu.au/deposit-your-data/license-reuse-data-agreement&rft_subject=eng&rft_subject=Hypersonic Propulsion and Hypersonic Aerodynamics&rft_subject=ENGINEERING&rft_subject=AEROSPACE ENGINEERING&rft_subject=Computational Fluid Dynamics&rft_subject=INTERDISCIPLINARY ENGINEERING&rft_subject=Turbulent Flows&rft.type=dataset&rft.language=English Access the data
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As part of NATO Advanced Vehicle Technology working group 352, Eilmer has been used to simulate a set of double cone experiments, to be compared with other codes and with experimental data from CUBRC.This dataset contains the entire set of Eilmer calculations run for AVT-352, including input files, grid generation scripts, log files, and converged flow field data. Post processing scripts are also provided, which are written in the python programming language.The github page linked above contains heat transfer and wall pressure predictions for all of the codes involved with AVT-352, Eilmer included.

Issued: 13 09 2024

Data time period: 2024 to 31 08 2024

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Subjects
Aerospace Engineering | Computational Fluid Dynamics | Engineering | Hypersonic Propulsion and Hypersonic Aerodynamics | Interdisciplinary Engineering | Turbulent Flows | eng |

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local : UQ:289097