Improved nonequilibrium viscous shock-layer scheme for hypersonic blunt-body flowfields
Author:
Affiliation:
1. VRA, Inc., Blacksburg, Virginia 24063
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26310
Reference30 articles.
1. A set of strongly coupled, upwind algorithms for computing flows in chemical nonequilibrium
2. On the computation of shock shapes in nonequilibrium hypersonic flows
3. Code calibration program in support of the Aeroassist Flight Experiment
Cited by 1 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. A new method for solution of viscous shock-layer equations;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2009-12-17
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