Wind-tunnel tests of ailerons at various speeds. : 3 - Ailerons of 0.20 airfoil chord and true contour with 0.35-aileron-chord Frise balance on the NACA 23012 airfoil / by W. Letko and W.B. Kemp.
Hinge moment, lift, and pressure-distribution measurements were made on a Frise aileron on an NACA 23012 airfoil in the two-dimensional test section of the LMAL stability tunnel. Speeds up to 360 miles per hour corresponding to a Mach number of about 0.470 were used. The nose radius of the aileron w...
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| Main Author: | |
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| Corporate Authors: | , |
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| Other title: | NACA Wartime Reports. Series L. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1943]
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| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L325. |
| Subjects: |
Norlin Library - Basement - Government Information - US
| Call Number: |
Y 3.N 21/5:11/L325
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| Y 3.N 21/5:11/L325 | Available Place a Hold |