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The Damping in Roll of Rocket-Powered Test Vehicles Having Rectangular Wings With NACA 65-006 and Symmetrical Double-Wedge Airfoil Sections of Aspect Ratio 4.5
| Author: | Dietz, Albert E. |
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| Year: | 1950 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L50B10 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58549/ |
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