Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil / by J.D. Bird.
An investigation has been made in two-dimensional flow to determine the effect of leakage past the aileron nose on the aerodynamic characteristics of ailerons. Plain and internally balanced ailerons of 0.20 airfoil chord were tested on an NACA 66(215)-216, a = 1.0 airfoil. The effects of amount and...
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| Main Author: | |
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| Corporate Authors: | , |
| Other title: | NACA Wartime Reports. Series L. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1945]
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| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L172. |
| Subjects: |
Norlin Library - Basement - Government Information - US
| Call Number: |
Y 3.N 21/5:11/L172
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| Y 3.N 21/5:11/L172 | Available Place a Hold |