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Wind tunnel investigation of control surface characteristics.12 - Various cover-plate alinements on the NACA 0015 airfoil with a 30 percent chord flap and large sealed internal balance
| Author: | Hoggard, H. Page. |
|---|---|
| Year: | 1943 |
| Document Type: | MAIN |
| Issuing Agency: | National Advisory Committee for Aeronautics, |
| SUDOC: | Y 3.N 21/5:11/L511 |
| Series: | Wartime Report / National Advisory Committee for Aeronautics ; |
| Report Number: | no. L511 |
| Subjects: | Plates (Engineering) |
| Charts, diagrams, etc | |
| Wind tunnel testing | |
| Flaps (Airplanes) | |
| Hinge moments (Aerodynamics) | |
| Aerofoils | |
| Airplanes--Control surfaces | |
| Link: | https://hdl.handle.net/2027/mdp.39015095014745 |
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