Hinge-moment characteristics of balanced elevator and rudder for a specific tail configuration on a fuselage in spinning attitudes /
The results of an investigation of a specific tail configuration in the Langley 15-foot free-spinning tunnel are presented in order to supplement the existing published data on hinge moments of elevators and rudders in spins. Hinge-moment measurements are presented for a balanced elevator equipped w...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1947
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
1400 |
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| Call Number: |
NACA TN 1400 |
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