Effect of horizontal-tail size and tail length on low-speed static longitudinal stability and damping in pitch of a model having 45 degrees sweptback wing and tail surfaces /
Wind-tunnel results of the effects of horizontal-tail size and length on the low-speed static longitudinal stability and the steady-state rotary damping in pitch for a complete model with wing and tail surfaces having the quarter-chord lines swept back 45 degrees and aspect ratios of 4 are presented
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1951
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2382 |
| Subjects: | |
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| Call Number: |
NACA TN 2382 |
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