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Effect of vertical location of a horizontal tail on the static longitudinal stability characteristics of a 45 degree sweptback-wing-fuselage combination of aspect ratio 8 at a Reynolds number of 4.0 x 10(exp 6)
| Author: | Salmi, Reino J. |
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| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L51J08 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59167/ |
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