Coefficient of drag of cylinders
Hi, i have a probleme with the drag's coefficient. I am with a 2-D axissymetric problem for a flow over a modified cylinder (a rocket). L=10m , D=0.5m and Mach=1.3
It seems that the probleme is the "reference value". I don't know the right value for the "Area" and the "Lenght". Can you help me ? Thank's |
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