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Authors

Author

Herbert W. Ridyard

Books

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
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

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