Flight determination of minimum drag of 0.11-scale rocket-boosted model of the Chance Vought XF8U-1 airplane with modified fuselage area distribution and faired inlet at Mach number from 0.82 to 1.68 : TED No. NACA DE 392
| Author: | Hastings, Earl C , Jr |
|---|---|
| Year: | 1955 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-SL55I27 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61719/ |