Span Load Distribution Resulting From Constant Vertical Acceleration for Thin Sweptback Tapered Wings With Streamwise Tips: Supersonic Leading and Trailing Edges
| Author: | Cole, Isabella J. |
|---|---|
| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3120 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57076/ |