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Longitudinal-control effectiveness and downwash characteristics at transonic speeds of a 1/30-scale semispan model of the Bell X-5 airplane as determined by the NACA wing-flow method
| Author: | Silsby, Norman S |
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| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L52K12 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59446/ |
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