Application of the multigrid solution solution technique to hypersonic entry vehicles
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Reference23 articles.
1. Predicted aerodynamics for a proposed personnel launch vehicle
2. HL-20 computational fluid dynamics analysis
3. Solution strategy for three-dimensional configurations at hypersonicspeeds
Cited by 4 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. Predictions of Heat Transfer in Hypersonic Viscous Flows by an Improved Third-Order WENO Scheme;Lecture Notes in Electrical Engineering;2019
2. Application of Gas-Kinetic BGK Scheme in Three-Dimensional Flow;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04
3. Computational Aerothermodynamic Design Issues for Hypersonic Vehicles;Journal of Spacecraft and Rockets;1999-01
4. Computational aerothermodynamic design issues for hypersonic vehicles;32nd Thermophysics Conference;1997-06-23
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