Drag characteristics of rectangular and swept-back NACA 65-009 airfoils having aspect ratios of 1.5 and 2.7 as determined by flight tests at supersonic speeds
| Author: | Alexander, Sidney R. |
|---|---|
| Year: | 1947 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L6J16 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58091/ |