 |
|
Preliminary wind-tunnel tests of triangular and rectangular wings in steady roll at Mach numbers of 1.62 and 1.92
| Author: | Brown, Clinton E |
|---|---|
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3740 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc56045/ |
Search developed and maintained by the University of Washington Libraries
Copyright 2010