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Scramjet intake

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The inflow conditions are

  • Mach =5.0
  • ρ=1.0
  • u=1.0
  • v=0.0

Geometry

Scramjet geometry

Density contours

Scramjet - Density contours

References

  • Kumar, A. (1981), "Numerical analysis of the scramjet-inlet flow field by using two-dimensional Navier-Stokes equations", Technical Paper 1940, NASA.
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