Wind-tunnel investigation of control-surface characteristics. : 20 - Plain and balanced flaps on an NACA 0009 rectangular semispan tail surface / by I. Elizabeth Garner.
Correlation is established between aerodynamic characteristics of control surfaces in two-dimensional and three-dimensional flow. Slope of lift curve was affected little by overhang and balance-nose shape, but increased by sealing flap-nose gap. Effectiveness of balancing tab was same for sealed pla...
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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,
[1944]
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Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L186. |
Subjects: |
Norlin Library - Basement - Government Information - US
Call Number: |
Y 3.N 21/5:11/L186
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Y 3.N 21/5:11/L186 | Available Place a Hold |