Determination of indicial lift and moment of a two-dimensional pitching airfoil at subsonic mach numbers from oscillatory coefficients with numerical calculations for a Mach number of 0.7
| Author: | Mazelsky, Bernard |
|---|---|
| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-2613 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc56169/ |