Minimum Drag of Four Versions of a Swept-Wing Fighter Airplane Obtained From Flight Tests of Rocket-Boosted Models at Mach Numbers From 0.81 to 1.71
| Author: | Hastings, Earl C., Jr. |
|---|---|
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L56E25A |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc53077/ |