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Unformatted text preview: 1 , 4 / mc c 1 , L , , , , 1 , cp x 2 , l c 2 , 4 / mc c 2 , L , and . Show what can you determine regarding the new values of , , 2 , cp x l c 4 / mc c L , and ? cp x Note: in recent years some students would assume a function for ( ) x z c and demonstrate the effects of one specific case. This falls far short of the goal here proving the impact of changes for all camber lines. Thus you are to work with the unknown and very general , not one example of . You do, however, assume that all airfoils under consideration satisfy the assumptions for thin airfoil theory. ( ) x z c ( ) x z c...
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- Fall '09