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Calculation of separated flows at subsonic and transonic speeds

  • John M. Klineberg
  • Joseph L. Steger
Conference paper
Part of the Lecture Notes in Physics book series (LNP, volume 19)

Keywords

Mach Number Inviscid Flow Turbulent Wake Displacement Thickness Viscous Layer 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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References

  1. Collins, D. J., private communication, April 1972, NASA Ames Research Center, Moffett Field, California.Google Scholar
  2. Klineberg, J. M., Kubota, T., and Lees, L., AIAA J. 10, pp. 581–588 (1972).ADSCrossRefGoogle Scholar
  3. Klineberg, J. M., and Lees, L., AIAA J. 7, pp. 2211–2221 (1969).ADSCrossRefGoogle Scholar
  4. Lees, L., and Reeves, B.L., AIAA J. 2, pp. 1907–1920 (1964).zbMATHMathSciNetCrossRefGoogle Scholar
  5. Pearcy, H. H., Osborne, J., and Haines, A. B., NPL Aero Note 1071, A.R.C. 30477 (1968).Google Scholar
  6. Steger, J. L., and Klineberg, J. M., AIAA paper 72–679 (1972).Google Scholar
  7. Steger, J. L., and Lomax, H., Lecture Notes in Physics, Vol. 8, pp. 193–197, Springer-Verlag, (1971).ADSCrossRefGoogle Scholar

Copyright information

© Springer-Verlag 1973

Authors and Affiliations

  • John M. Klineberg
    • 1
  • Joseph L. Steger
    • 1
  1. 1.Ames Research CenterNASAMoffett FieldUSA

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