Reduction of profile drag at supersonic velocities by the use of airfoil sections having a blunt trailing edge
| Author: | Chapman, Dean R. |
|---|---|
| Year: | 1955 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3503 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57509/ |