Drag Measurements of a 34 Degree Swept-Forward and Swept-Back NACA 65-009 Airfoil of Aspect Ratio 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-L6I11 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58039/ |