Code verification and numerical error estimation for use in model validation of laminar, hypersonic double-cone flows-Reference-Cited by-同舟云学术

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Code verification and numerical error estimation for use in model validation of laminar, hypersonic double-cone flows

Published:2019-01-06 Issue: Volume: Page:
ISSN:
Container-title:AIAA Scitech 2019 Forum
language:
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Author:

Carnes Brian¹,Weirs V. G.¹,Smith Thomas¹

Affiliation:

1. Sandia National Laboratories

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2019-2175

Reference18 articles.

1. Experimental studies of laminar separated flows induced by shock wave/boundary layer and shock/shock interaction in hypersonic flows for CFD validation

2. Numerical and Experimental Characterization of High Enthalpy Flow in an Expansion Tunnel Facility

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. An Assessment of the Laminar Hypersonic Double-Cone Experiments in the LENS-XX Tunnel;AIAA Journal;2023-08

2. Adaptive Model Reduction of High-Order Solutions of Compressible Flows via Optimal Transport;International Journal of Computational Fluid Dynamics;2023-07-03

3. Verification Study of the Multi-Fidelity Toolkit;AIAA SCITECH 2022 Forum;2022-01-03

4. Code-verification techniques for hypersonic reacting flows in thermochemical nonequilibrium;Journal of Computational Physics;2021-01

5. Code-Verification Techniques for Hypersonic Reacting Flow in Thermochemical Nonequilibrium;AIAA Aviation 2019 Forum;2019-06-14

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