Laminar near wake of a circular cylinder at hypersonic speeds
Subscripts b= base d= dividing streamline e= outer edge of boundary layer eq= equilibrium
est= flow establishment N= nitrogen O= oxygen o= total conditions r= reattachment point
sep= separation point stag= front stagnation point w= body wall 1= conditions ahead of bow
shock/freestream 2= conditions behind bow shock 3= inviscid flow outside free shear layer
4= inviscid flow behind wake recompression shock
est= flow establishment N= nitrogen O= oxygen o= total conditions r= reattachment point
sep= separation point stag= front stagnation point w= body wall 1= conditions ahead of bow
shock/freestream 2= conditions behind bow shock 3= inviscid flow outside free shear layer
4= inviscid flow behind wake recompression shock
Subscripts b= base d= dividing streamline e= outer edge of boundary layer eq= equilibrium est= flow establishment N= nitrogen O= oxygen o= total conditions r= reattachment point sep= separation point stag= front stagnation point w= body wall 1= conditions ahead of bow shock/freestream 2= conditions behind bow shock 3= inviscid flow outside free shear layer 4= inviscid flow behind wake recompression shock
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