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Effect of Fuselage Interference on the Damping in Roll of Delta Wings of Aspect Ratio 4 in the Mach Number Range Between 0.6 and 1.6 as Determined With Rocket Propelled Vehicles
| Author: | Bland, William M., Jr. |
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| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L52E13 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59225/ |
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