Effect of changing the mean camber of an airfoil section (1924)
NASA Technical Reports Server (NTRS) · leaf 34
A-Tneorctical biconvux airfoil B=Initial discontinuity C=Cz,„teOaJ4-0 o/c, i =^0,9 2o/c Vaxiations of.Cg-Cg plotted against o/ o /)C2=6.55 Ao/c Fig. 6 Effect of maximum camber o/c on Cg.Results for Devvoitine air- foils (S.T.Ae.25A to 2SA)
NASA Technical Reports Server (NTRS)
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