Theoretical calculation of the pressure distribution, span loading, and rolling moment due to sideslip at supersonic speeds for thin sweptback tapered wings with supersonic trailing edges and wing tips parallel to the axis of wing symmetry
| Author: | Margolis, Kenneth |
|---|---|
| Additional Authors: | Sherman, Windsor L. |
| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-2898 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57003/ |