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A numerical solution of the planar supersonic near-wake with its error analysis

  • B. B. Ross
  • S. I. Cheng
Session III Boundary Layers
Part of the Lecture Notes in Physics book series (LNP, volume 8)

Keywords

Wall Boundary Condition Outflow Boundary Rear Stagnation Point Rear Boundary Recompression Shock 
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. Allen, J.S., and Cheng, S.I., Physics of Fluids 13,37-52 (1970); also, Allen, J.S., Ph.D. Thesis, Princeton University (1968).Google Scholar
  2. Cheng, S.I., Physics of Fluids, Supplement II, 34–41 (1969).Google Scholar
  3. Cheng, S.I., AIAA Preprint No. 70-2 (1970); final manuscript to appear in AIAA J. Google Scholar
  4. Kreiss, H.O., and Lundqvist, E., Math. Comp. 22, 1–12 (1968)Google Scholar
  5. Moretti, G., Physics of Fluids, Supplement II, 13–20 (1969).Google Scholar
  6. Roache, P.J., and Mueller, T.J., AIAA J. 8 530–538 (1970).Google Scholar
  7. Ross, B.B., Ph.D. Thesis, Princeton University (Dec., 1970)Google Scholar

Copyright information

© Springer-Verlag 1971

Authors and Affiliations

  • B. B. Ross
    • 1
  • S. I. Cheng
    • 1
  1. 1.Princeton UniversityPrinceton

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