CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Wiki > Scramjet intake

Scramjet intake

From CFD-Wiki

(Difference between revisions)
Jump to: navigation, search

Revision as of 08:07, 19 September 2005

The inflow conditions are

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

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.
My wiki