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Aerodynamic characteristics at transonic and supersonic speeds of a rocket-propelled airplane configuration having a 52.5 degree delta wing and a low, swept horizontal tail
| Author: | Kehlet, Alan B |
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| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L54A20 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc60270/ |
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