Use of Pade fractions in the calculation of blunt body flows
- 1 July 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (7), 1431-1433
- https://doi.org/10.2514/3.6378
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
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- Computational aspects of the detached shock problem.AIAA Journal, 1968
- A conformal mapping approach to the blunt body problem.AIAA Journal, 1967
- Use of rational approximations in the calculation of flows past blunt bodies.AIAA Journal, 1967
- Methods and applications of power seriesMathematics of Computation, 1966
- An experimental investigation of the shock layer surrounding a sphere in supersonic flowAIAA Journal, 1965
- The Use of Rational Approximations in the Calculation of Flows with Detached ShocksJournal of the Aerospace Sciences, 1960
- A model of supersonic flow past blunt axisymmetric bodies, with application to Chester's solutionJournal of Fluid Mechanics, 1957