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Longitudinal Stability and Control Characteristics of a Semispan Airplane Model With a Swept-Back Tail From Tests at Transonic Speeds by the NACA Wing-Flow Method
| Author: | Zalovcik, John A. |
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| Year: | 1947 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L6K21 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58081/ |
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