 |
|
Thin airfoil theory based on approximate solution of the transonic flow equation
| Author: | Spreiter, John R. |
|---|---|
| Year: | 1957 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3970 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc56291/ |
Search developed and maintained by the University of Washington Libraries
Copyright 2010