 |
|
A study of the flow over a 45 degree sweptback wing-fuselage combination at transonic Mach numbers
| Author: | Whitcomb, Richard T |
|---|---|
| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L52D01 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59381/ |
Search developed and maintained by the University of Washington Libraries
Copyright 2010