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Free-flight investigation over a Mach number range from 0.74 to 1.43 at lift coefficients from minus 0.15 to 0.75 of an airplane-configuration model having a 52.5 degree delta wing and a low swept horizontal tail
| Author: | Kehlet, Alan B |
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| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L56G09 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc62545/ |
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