Flight investigation at Mach numbers from 0.6 to 1.7 to determine drag and base pressures on a blunt trailing-edge airfoil and drag of diamond and circular-arc airfoils at zero lift
| Author: | Morrow, John D |
|---|---|
| Year: | 1955 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3548 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57805/ |