Viscous Hypersonic Flow Past Blunted Cones at Small Angles of Attack
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.60755
Reference8 articles.
1. Calculation of the flow on a blunted cone at high angle of attack
Cited by 10 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. Efficient numerical method for simulation of supersonic viscous flow past a blunted body at a small angle of attack;Computers & Fluids;1994-01
2. Application of the small-parameter method to the problem of the spatial flow of a viscous gas past bodies;Journal of Applied Mathematics and Mechanics;1992-01
3. Calculation of the flow field past spherically blunted cones near the plane of symmetry for various shock layer flow regimes with insufflation of gas from the surface;Journal of Applied Mechanics and Technical Physics;1992
4. On the theory of a three-dimensional, viscous hypersonic shock layer in the neighbourhood of the plane of symmetry;Journal of Applied Mathematics and Mechanics;1984-01
5. Galileo Probe Forebody Flowfield Predictions;Entry Vehicle Heating and Thermal Protection Systems: Space Shuttle, Solar Starprobe, Jupiter Galileo Probe;1983-01-01
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