Wind-tunnel investigation of a beveled aileron shape designed to increase the useful deflection range / by R.T. Jones and W.J. Underwood.
The useful range of deflection of a control surface is ordinarily limited by the occurrence of flow separation on the convex side of the surface behind the hinge. After this separation occurs the hinge moment increases rapidly, making it extremely difficult to deflect the aileron beyond this point a...
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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,
[1944]
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| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L651. |
| Subjects: |
Norlin Library - Basement - Government Information - US
| Call Number: |
Y 3.N 21/5:11/L651
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| Y 3.N 21/5:11/L651 | Available Place a Hold |