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A Method for Calculating the Subsonic Steady-State Loading on an Airplane With a Wing of Arbitrary Plan Form and Stiffness
| Author: | Gray, W. L. |
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| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3030 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57009/ |
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