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Effect of elevator-profile modifications and trailing-edge strips on elevator hinge-moment and other aerodynamic characteristics of a full-scale horizontal tail surface

Tests of a full-scale horizontal tail surface in the Langley 16-foot high-speed tunnel

Pressure-distribution measurements on a full-scale horizontal tail surface for a Mach number range of 0.20 to 0.70

Published Year

• 1940-1949 (3) *

Author

• Schueller, Carl F. (3) *
• Korycinski, Peter F. (2)

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