Investigation of symmetric body indentations designed to reduce the transonic zero-lift wave drag of a 45 degree swept wing with an NACA 64A006 section and with a thickened leading-edge section
| Author: | Holdaway, George H |
|---|---|
| Year: | 1957 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A56K26 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc63309/ |
