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Hypersonic perfect-gas flow past an axisymmetric blunt body with a narrow groove in its frontal surface

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Abstract

The features of the flowfield and heat transfer on the surface of an axisymmetric body with a narrow groove in its nose immersed in a hypersonic perfect-gas stream (M∞=6.1) are studied on the basis of a numerical analysis of the two-dimensional Navier-Stokes equations. The calculations are performed for both thermally insulated and isothermal surfaces having grooves of different width. The calculated results are compared with experimental data.

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References

  1. I. Yegorov, V. Bashkin, E. Buldakov, and D. Ivanov, “Hypersonic flow over flat plate and Mars Pathfinder with gaps in its surfaces,” in:21st Intern. Symp. on Space Technology and Science. Sonic City. Omiya, Japan, 1998.

  2. B. L. Haas and E. Venkatapathy, “Mars Pathfinder computations including base-heating predictions,” in:30th AIAA Thermophysics Conf., San Diego, 1995, AIAA Paper No. 95-2086, p. 1.

  3. I. Yu. Babaev, V. A. Bashkin, and I. V. Egorov, “Numerical solution of the Navier-Stokes equations using iterative methods of variational type,”Zh. Vych. Mat. Mat. Fiz.,34, 1693 (1994).

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  4. V. A. Bashkin, I. V. Egorov, and D. V. Ivanov, “Application of Newton’s method to the calculation of internal supersonic separated flows,”Zh. Prikl. Mekh. Tekhn. Fiz., No. 1, 30 (1997).

  5. V. Ya. Borovoy, V. N. Brazhko, G. I. Maikapar,et al., “Heat transfer peculiarities in supersonic flows,”J. Aircraft,29, 969 (1992).

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Authors
  1. V. A. Bashkin
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  2. I. V. Egorov
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  3. D. V. Ivanov
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  4. A. S. Skuratov
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Additional information

Moscow. Translated from Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, No. 1, pp. 117–124, January–February, 2000.

The study was carried out with the support of the International Scientific and Technical Center (project No. 036).

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Bashkin, V.A., Egorov, I.V., Ivanov, D.V. et al. Hypersonic perfect-gas flow past an axisymmetric blunt body with a narrow groove in its frontal surface. Fluid Dyn 35, 95–100 (2000). https://doi.org/10.1007/BF02698793

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  • DOI: https://doi.org/10.1007/BF02698793

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