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Search: Posts Made By: Amiga500
Forum: Main CFD Forum August 3, 2009, 13:00
Replies: 1
Views: 1,772
Posted By Amiga500
Pt/P = {1+ [((gamma-1)/2)*Mach^2]}...

Pt/P = {1+ [((gamma-1)/2)*Mach^2]} ^(gamma/[gammma-1])

Pt = Total pressure
P = Static pressure
gamma = ratio of specific heats (1.4 for air)
Mach = Mach number


Change your static pressure,...
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