 |
|
Effects of a Fuselage and Various High-Lift and Stall-Control Flaps on Aerodynamic Characteristics in Pitch of an NACA 64-Series 40 Degree Swept-Back Wing
| Author: | Conner, D. William |
|---|---|
| Year: | 1947 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L6L27 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58167/ |
Search developed and maintained by the University of Washington Libraries
Copyright 2010