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Chapter:
Boundary-Layer-Theory
Some Important Formulaes:
For laminar flow,
`delta/x =4.64/root ()(R_e`
Friction factor, `f=64/R_e`
`tau_0=3/2 (mu*U_0)/delta`
`C_D=1.292/root ()(R_e)`
For Turbulent flow:
`delta/x=0.371/(R_e)^(1/5)`
`C_D=0.072/(R_e)^(1/5)`
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