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Search: Posts Made By: SergeAS
Forum: Main CFD Forum April 14, 2012, 07:30
Replies: 11
Views: 3,883
Posted By SergeAS
This problem does not consider the thermal state...

This problem does not consider the thermal state of the sphere itself. Temperature on my pics corresponds only to the temperature of boundary layer of gas (air) assuming no heat transfer between the...
Forum: Main CFD Forum April 13, 2012, 18:35
Replies: 11
Views: 3,883
Posted By SergeAS
Quick assessment of temperature behind the shock...

Quick assessment of temperature behind the shock wave can be obtained from the relation
\cfrac{T_{2}}{T_{1}} \approx\cfrac{2\gamma(\gamma-1)}{(\gamma+1)^{2}}M_{1}^{2} In stagnation point behind bow...
Forum: Main CFD Forum April 6, 2012, 16:37
Replies: 11
Views: 3,883
Posted By SergeAS
diameter and mach number - Yes. BC - No Inlet...

diameter and mach number - Yes.
BC - No
Inlet and top side - freestream BC
Outlet - zero gradient in X direction
Wall of sphere - no-sleep BC (wall assumed adiabatic)
bottom side - axisymmetric...
Forum: Main CFD Forum April 2, 2012, 10:41
Replies: 11
Views: 3,883
Posted By SergeAS
You want know all my secrets ? :) It is...

You want know all my secrets ? :)

It is blended (CD-LxF) scheme with locally adapted blending factor
Forum: Main CFD Forum April 2, 2012, 10:17
Replies: 11
Views: 3,883
Posted By SergeAS
This problem is widely studied since the early...

This problem is widely studied since the early 60s of last century and you can easily find a large number of publications on this topic. In addition modern advanced CFD codes for compressible flows...
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