Scramjet intake
From CFD-Wiki
(Difference between revisions)
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
References
- Kumar, A. (1981), "Numerical analysis of the scramjet-inlet flow field by using two-dimensional Navier-Stokes equations", Technical Paper 1940, NASA.
