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: | 1949 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L8L30 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57969/ |