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Supersonic viscous flow over cones at incidence

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Sixth International Conference on Numerical Methods in Fluid Dynamics

Part of the book series: Lecture Notes in Physics ((LNP,volume 90))

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Abstract

The conically symmetric Navier-Stokes equations are solved by MacCormack's method for the supersonic flow past sharp cones at incidence. To provide closure for the case of turbulent flows, a scalar eddy-viscosity model based on mixing length hypotheses is used. The results are compared with available experimental data.

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References

  1. Daywitt, J., Anderson, D., and Kutler, P., AIAA 15th Aerospace Sciences Meeting. 1977, Paper 77-86.

    Google Scholar 

  2. Miyazawa, M., Proceedings 10th International Symposium on Space Technology and Science, Tokyo, 1973, pp. 433–442.

    Google Scholar 

  3. Stetson K. F., ARL 71-0127, Aerospace Research Laboratories, Wright-Patterson AFB, Ohio, August 1971.

    Google Scholar 

  4. R. F. Feldhun, AIAA J., 9, 1971, pp. 1074–1081.

    Google Scholar 

  5. McRae, D. S., AFFDL-TR-76-139, Air Force Flight Dynamics Laboratory, Wright-Patterson AFB, Ohio, 1976.

    Google Scholar 

  6. Harris, J. E. and Morris, D. J., Proceedings 4th International Conference on Numerical Methods in Fluid Dynamics, 1974, Lecture Notes in Physics No. 35, pp. 204–211.

    Google Scholar 

  7. Rainbird, W. J., AGARD Conference Proceedings No. 30, AGARD Specialists Meeting on Hypersonic Boundary Layers and Flow Fields, London, May 1-3, 1968, pp. 19-1 to 19-19.

    Google Scholar 

  8. McElderry, E. D., Jr., AFFDL TM-74-170, Air Force Flight Dynamics Laboratory, 1974.

    Google Scholar 

  9. Shang, J. S., Hankey, W. L., and Law, C. H., AIAA J., 14, 1976, pp. 1451–1457.

    Google Scholar 

  10. MacCormack, R. W., AIAA Paper 69-354, 1969.

    Google Scholar 

  11. Tracy, R. R., California Institute of Technology, Aeronautical Laboratories Memorandum No. 69, 1963.

    Google Scholar 

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Author information

Author notes

  1. M. Y. Hussaini

    Present address: ICASE, Langley Research Center, NASA, USA

Authors and Affiliations

  1. Air Force Flight Dynamics Laboratory, Ames Research Center, NASA, Moffett Field, California

    Major David S. McRae

  2. Ames Research Center, NASA, Moffett Field, California

    M. Y. Hussaini

Authors
  1. Major David S. McRae
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  2. M. Y. Hussaini
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Editor information

H. Cabannes M. Holt V. Rusanov

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© 1979 Springer-Verlag

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McRae, D.S., Hussaini, M.Y. (1979). Supersonic viscous flow over cones at incidence. In: Cabannes, H., Holt, M., Rusanov, V. (eds) Sixth International Conference on Numerical Methods in Fluid Dynamics. Lecture Notes in Physics, vol 90. Springer, Berlin, Heidelberg. https://doi.org/10.1007/3540091157_192

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  • DOI: https://doi.org/10.1007/3540091157_192

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  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-09115-8

  • Online ISBN: 978-3-540-35521-2

  • eBook Packages: Springer Book Archive

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