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Aerodynamic characteristics of a wing with quarter-chord line swept back 35©�, aspect ratio 6, taper ratio 0.6, and NACA 65A006 airfoil section.Transonic-bump method
| Author: | Sleeman, William C. |
|---|---|
| Additional Authors: | Morrison, William D. |
| Year: | 1949 |
| Document Type: | NACA |
| Issuing Agency: | National Advisory Committee for Aeronautics, |
| SUDOC: | Y 3.N21/5:15/L9K10a |
| Series: | National Advisory Committee for Aeronautics research memorandum ; |
| Report Number: | L9K10a |
| Subjects: | Lift (Aerodynamics) |
| Airplanes--Wings | |
| Pitching (Aerodynamics) | |
| Drag (Aerodynamics) | |
| Airplanes--Fuselage | |
| Aerodynamics, Transonic | |
| Airplanes--WIngs | |
| Link: | https://hdl.handle.net/2027/mdp.39015086464610 |
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