Langley 9-inch supersonic tunnel tests of several modifications of a supersonic missile having tandem cruciform lifting surfaces : three-component data results of models having ratios of wing span to tail span equal to 1
| Author: | Rainey, Robert W |
|---|---|
| Year: | 1951 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L9L30 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58609/ |