 |
|
Influence of airfoil trailing-edge angle and trailing-edge-thickness variation on the effectiveness of a plain flap at high subsonic Mach numbers
| Author: | Hemenover, Albert D |
|---|---|
| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3174 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57077/ |
Search developed and maintained by the University of Washington Libraries
Copyright 2010