Effect of horizontal tail on low-speed static lateral stability characteristics of a model having 45 degree sweptback wing and tail surfaces /
This report contains wind-tunnel results of the effect of change in horizontal-tail size and location on the static-lateral-stability parameters for a complete mode with wing and tail surfaces having the quarter-chord line swept back 45 degrees. Charts applicable to the design of similar tail config...
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| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. :
National Advisory Committee for Aeronautics,
1950
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2010 |
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