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The Effect of a Change in Airfoil Section on the Hinge-moment Characteristics of a Half-delta Tip Control with a 60© Sweep Angle at a Mach Number of 6.9
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The Effect of a Change in Airfoil Section on the Hinge-moment Characteristics of a Half-delta Tip Control with a 60© Sweep Angle at a Mach Number of 6.9

David E. Fetterman, Herbert W. Ridyard — 1954
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