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searching for Slender-body theory 1 found (7 total)

Aerodynamic potential-flow code (1,541 words) [view diff] no match in snippet view article find links to article

{\displaystyle C_{p}=1-|{\vec {V}}|^{2}+M_{\infty }^{2}u^{2}} The Slender Body Theory Pressure Coefficient is: C p = − ( 2 u + v 2 + w 2 ) {\displaystyle