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We'll next create the bottom edge corresponding to the nozzle wall. This edge is curved. Since
A = Πr2
where r
( x ) is the radius of the cross-section at x and
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for the given nozzle geometry, we get
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r( x ) = \[(0.1 + x{^}2^)/*Π*\]^0.5^; \-0.5 < x < 0.5 |
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