David E. Fetterman

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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

Comparison of Full-scale Lift and Drag Characteristics of the X-15 Airplane with Wind-tunnel Results and Theory

Comparison of Full-scale Lift and Drag Characteristics of the X-15 Airplane with Wind-tunnel Results and Theory

Edward J. Hopkins, David E. Fetterman, Edwin J. Saltzman

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