Flight Investigation of the Supersonic Area Rule for a Straight Wing-Body Configuration at Mach Numbers Between 0.8 and 1.5
| Author: | Hoffman, Sherwood |
|---|---|
| Additional Authors: | Wolff, Austin L. |
| Year: | 1955 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L55C09 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61224/ |