Use of Pade fractions in the calculation of blunt body flows
Author:
Affiliation:
1. U. S. Naval Ordnance Laboratory, Silver Spring, Md.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6378
Reference15 articles.
1. Use of rational approximations in the calculation of flows past blunt bodies.
2. A model of supersonic flow past blunt axisymmetric bodies, with application to Chester's solution
3. The Use of Rational Approximations in the Calculation of Flows with Detached Shocks
4. Initial Stages of Axisymmetric Shock-on-Shock Interaction for Blunt Bodies
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1. The use of Pade fractions in the calculation of nozzle flows;Padé Approximants Method and Its Applications to Mechanics;1976
2. Application of methods for acceleration of convergence to the calculation of singularities of transonic flows;Padé Approximants Method and Its Applications to Mechanics;1976
3. Calculation of nozzle flows using Pade fractions.;AIAA Journal;1973-04
4. Least-squares solution for the blunt body hypersonic flow problem;Journal of Computational Physics;1972-10
5. Modern advances in the physics of gasdynamic lasers;10th Aerospace Sciences Meeting;1972-01-17
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