Scramjet intake

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Revision as of 08:07, 19 September 2005 (view source) Praveen (Talk | contribs) ← Older edit		Latest revision as of 08:19, 19 September 2005 (view source) Praveen (Talk | contribs)
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	* u=1.0		* u=1.0
	* v=0.0		* v=0.0
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		+	==Geometry==
		+
		+	[[Image:Vtc_scramjet_geometry.png | Scramjet geometry]]
	==Density contours==		==Density contours==

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Latest revision as of 08:19, 19 September 2005

The inflow conditions are

• Mach =5.0
• ρ=1.0
• u=1.0
• v=0.0

Geometry

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.