Unformatted text preview: 1 , 4 / mc c 1 , L α , , , , 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
- Airfoil, Zc, airfoil camber, quarter-chord moment coefficients, general zc