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Wind tunnel pressure distribution tests on a series of biplane wing models Part II : effects of changes in decalage, dihedral, sweepback and overhang (1929)

NASA Technical Reports Server (NTRS) · leaf 19

An illustration from Wind tunnel pressure distribution tests on a series of biplane wing models Part II : effects of changes in decalage, dihedral, sweepback and overhang, 1929, leaf 19
Angle of attack,d Fig.14 Effect of dihedral on lower wing coefficient of normal force.

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