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Stability and drag characteristics of 1/10-scale model of the Convair XF2Y-1 airplane with open inlets containing boundary layer splitter plates as obtained in free flight at Mach numbers between 0.7 and 1.5 : TED No. NACA DE 365
| Author: | Bland, William M , Jr |
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| Year: | 1955 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-SL55D14 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61248/ |
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