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An implicit finite difference method for chemical nonequilibrium flow through an axisymmetric supersonic nozzle

  • Kazuhiro Nakahashi
Contributed Papers
Part of the Lecture Notes in Physics book series (LNP, volume 170)

Keywords

Nozzle Wall Operational Count Fluid Dynamic Equation Rocket Nozzle National Aerospace Laboratory 
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References

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    Nickerson, G. R., Coats, D. E. and Bartz, J. L., NASA CR-152999, 1977.Google Scholar
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    Ratliff, A. W., NASA CR-3121, 1979.Google Scholar
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    Nakahashi, K., Kisara, K., Moro, A. and Miyajima, H., in Proc. of 24th Space Science and Technology, Japan, 1980.Google Scholar
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    Stiles, R. J. and Hoffman, J. D., AIAA Paper No.81–1432, 1981.Google Scholar
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    Kliegel, J. R. and Levine, J. N., AIAA J., Vol.7, No.7, pp.1375–1378, 1969.Google Scholar
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    Nakahashi, K., Moro, A. and Miyajima, H., Technical Report of National Aerospace Laboratory, Japan, NAL TR-634, 1980.Google Scholar
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    Isaacson, E. and Keller, H. B., “Analysis of Numerical Methods”, John Weley & Sons, 1966Google Scholar
  8. 8).
    Miyajima, H. et al., Technical Report of National Aerospace Laboratory, Japan, NAL TR-662, 1981.Google Scholar

Copyright information

© Springer-Verlag 1982

Authors and Affiliations

  • Kazuhiro Nakahashi
    • 1
  1. 1.National Aerospace Laboratory MiyagiJapan

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