author: warren a tucker

Characteristics of Thin Triangular Wings with Triangular-tip Control Surfaces at Supersonic Speeds with Mach Lines Behind the Leading Edge

... Imax –。。ru 2 ( 1 – cos2ß1 ) dr - or = πr U max22sin21 CD = 2 sin sin232 ( 5 ) B1 . Then the ( 6 ) ( 7 ) Equation ( 6 ) is identical with Epstein's result ( reference 7 ) . Since Epstein neglected the effect of the pressure drop due to ...

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