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Effect of fuselage length and a canopy on the static longitudinal and lateral stability characteristics of 45 degrees sweptback airplane models having fuselages with square cross sections
| Author: | Jaquet, Byron M. |
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| Year: | 1957 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3961 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc56342/ |
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