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Ferreyra, R.T.; Tamagno, J.P.;

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Recently, some new analytical methods have been developed and successfully applied to provide solutions for the Taylor-Maccoll boundary value problem. In this paper an analysis is carried out to justify the generation of crossing regions for lower cone angles. To this end, a key formulation between the free stream Mach number, the geometric cone angle and the shock wave properties, is provided.

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Palavras-chave: Shock wave, Cones, Compressible flow,


DOI: 10.5151/meceng-wccm2012-19649

Referências bibliográficas
  • [1] Taylor, G.I. Andamp; Maccoll, J.W. ‘The air pressure on a cone moving at high speeds’, Procee-dings of the Royal Society of London, Series A, London, vol. 139, pp. 278-29, 1933.
  • [2] Anderson, J.D., ‘Modern Compressible Flow with Historical Perspective’, Mc Graw Hill, Series in aeronautical and aerospace engineering, 3rd edition, New York, pp. 1-375., 2003
  • [3] Ferreyra, RT Andamp; Tamagno, J. P. ‘A non local technique to approach the solutions of nonli-near boundary value problems applied to a supersonic flow model’, International Federa-tion of Nonlinear Analysis IFNA-ANS scientific Journal ‘Problems of nonlinear Analysis in Engineering Systems’, 2012, (manuscript sent for Special Issue 2012).
  • [4] Ferreyra, R. T. ‘New closed form solutions for Taylor and Maccoll Model’, Journal of Fluid Mechanics, (sent for publication 2012), 2012.
Como citar:

Ferreyra, R.T.; Tamagno, J.P.; "CROSSING REGIONS FOR SUPERSONIC CONES", p. 3999-4002 . In: In Proceedings of the 10th World Congress on Computational Mechanics [= Blucher Mechanical Engineering Proceedings, v. 1, n. 1]. São Paulo: Blucher, 2014.
ISSN 2358-0828, DOI 10.5151/meceng-wccm2012-19649

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