Investigation of the aerodynamic characteristics in pitch and sideslip of a 45©� swept-wing airplane configuration with various vertical locations of the wing and horizontal tail.Static lateral and directional stability; Mach numbers of 1.41 and 2.01
| Author: | Spearman, M. Leroy. |
|---|---|
| Additional Authors: | Robinson, Ross B. |
| Year: | 1957 |
| Document Type: | NACA |
| Issuing Agency: | National Advisory Committee for Aeronautics, |
| SUDOC: | Y 3.N 21/5:15/L57J25A |
| Series: | NACA research memorandum ; |
| Report Number: | L57J25A |
| Subjects: | Charts, diagrams, etc |
| Wind tunnel testing | |
| Mach number | |
| Pitching (Aerodynamics) | |
| Airplanes--Wings, Swept-back | |
| Airplanes--Tail surfaces | |
| Stability of airplanes, Lateral | |
| Link: | https://hdl.handle.net/2027/mdp.39015086466235 |