Computational aspects of the detached shock problem.
Author:
Affiliation:
1. University of Minnesota, Minneapolis, Minn.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4677
Reference8 articles.
1. A model of supersonic flow past blunt axisymmetric bodies, with application to Chester's solution
2. A conformal mapping approach to the blunt body problem.
3. Use of rational approximations in the calculation of flows past blunt bodies.
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. Application of methods for acceleration of convergence to the calculation of singularities of transonic flows;Padé Approximants Method and Its Applications to Mechanics;1976
2. Series solution for the planar asymmetric blunt-body problem;Physics of Fluids;1975
3. Use of Pade fractions in the calculation of blunt body flows;AIAA Journal;1971-07
4. Initial Stages of Axisymmetric Shock-on-Shock Interaction for Blunt Bodies;Physics of Fluids;1970
5. Diffraction of a plane shock by an analytic blunt body;Journal of Fluid Mechanics;1969-08-14
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