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The aerodynamic properties of thick aerofoils suitable for internal bracing (1920)

NASA Technical Reports Server (NTRS) · leaf 9

An illustration from The aerodynamic properties of thick aerofoils suitable for internal bracing, 1920, leaf 9 — »45 MAXIMUM SECT/ON NORMAL TO CHOffO full Six* Ch«r4'3' FlQUBE 10 144374—20 2

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