Development of lattice Boltzmann flux solver for simulation of hypersonic flow past flight vehicles

10.1088/1742-6596/1053/1/012073

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Bibliographic Details
Main Authors: Meng, Z, Yang, L, Shu, C, Hu, F, Wang, D, Zhang, W
Other Authors: MECHANICAL ENGINEERING
Format: Conference or Workshop Item
Published: 2020
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Online Access:https://scholarbank.nus.edu.sg/handle/10635/178076
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Institution: National University of Singapore
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spelling sg-nus-scholar.10635-1780762024-11-09T04:22:36Z Development of lattice Boltzmann flux solver for simulation of hypersonic flow past flight vehicles Meng, Z Yang, L Shu, C Hu, F Wang, D Zhang, W MECHANICAL ENGINEERING Finite volume method Flight simulators Hypersonic flow Hypersonic vehicles Inductively coupled plasma mass spectrometry One dimensional Shock waves Central difference method Computational robustness Flight vehicles Lattice boltzmann Numerical dissipation One-dimensional lattice Strong shock waves Switch function Navier Stokes equations 10.1088/1742-6596/1053/1/012073 Journal of Physics: Conference Series 1053 1 12073 2020-10-20T05:01:25Z 2020-10-20T05:01:25Z 2018 Conference Paper Meng, Z, Yang, L, Shu, C, Hu, F, Wang, D, Zhang, W (2018). Development of lattice Boltzmann flux solver for simulation of hypersonic flow past flight vehicles. Journal of Physics: Conference Series 1053 (1) : 12073. ScholarBank@NUS Repository. https://doi.org/10.1088/1742-6596/1053/1/012073 17426588 https://scholarbank.nus.edu.sg/handle/10635/178076 Attribution 4.0 International http://creativecommons.org/licenses/by/4.0/ Unpaywall 20201031
institution National University of Singapore
building NUS Library
continent Asia
country Singapore
Singapore
content_provider NUS Library
collection ScholarBank@NUS
topic Finite volume method
Flight simulators
Hypersonic flow
Hypersonic vehicles
Inductively coupled plasma mass spectrometry
One dimensional
Shock waves
Central difference method
Computational robustness
Flight vehicles
Lattice boltzmann
Numerical dissipation
One-dimensional lattice
Strong shock waves
Switch function
Navier Stokes equations
spellingShingle Finite volume method
Flight simulators
Hypersonic flow
Hypersonic vehicles
Inductively coupled plasma mass spectrometry
One dimensional
Shock waves
Central difference method
Computational robustness
Flight vehicles
Lattice boltzmann
Numerical dissipation
One-dimensional lattice
Strong shock waves
Switch function
Navier Stokes equations
Meng, Z
Yang, L
Shu, C
Hu, F
Wang, D
Zhang, W
Development of lattice Boltzmann flux solver for simulation of hypersonic flow past flight vehicles
description 10.1088/1742-6596/1053/1/012073
author2 MECHANICAL ENGINEERING
author_facet MECHANICAL ENGINEERING
Meng, Z
Yang, L
Shu, C
Hu, F
Wang, D
Zhang, W
format Conference or Workshop Item
author Meng, Z
Yang, L
Shu, C
Hu, F
Wang, D
Zhang, W
author_sort Meng, Z
title Development of lattice Boltzmann flux solver for simulation of hypersonic flow past flight vehicles
title_short Development of lattice Boltzmann flux solver for simulation of hypersonic flow past flight vehicles
title_full Development of lattice Boltzmann flux solver for simulation of hypersonic flow past flight vehicles
title_fullStr Development of lattice Boltzmann flux solver for simulation of hypersonic flow past flight vehicles
title_full_unstemmed Development of lattice Boltzmann flux solver for simulation of hypersonic flow past flight vehicles
title_sort development of lattice boltzmann flux solver for simulation of hypersonic flow past flight vehicles
publishDate 2020
url https://scholarbank.nus.edu.sg/handle/10635/178076
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