September 18, 2013 Presentation Open Access

Obert, Ed

DCAT Export

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    <dct:title>Static Directional Stability and Control of Transport Aircraft</dct:title>
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    <dcat:keyword>stability</dcat:keyword>
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    <dcat:keyword>control</dcat:keyword>
    <dcat:keyword>transport</dcat:keyword>
    <dcat:keyword>aircraft</dcat:keyword>
    <dcat:keyword>side force</dcat:keyword>
    <dcat:keyword>yaw</dcat:keyword>
    <dcat:keyword>sideslip</dcat:keyword>
    <dcat:keyword>wind tunnel</dcat:keyword>
    <dcat:keyword>tail</dcat:keyword>
    <dcat:keyword>wing</dcat:keyword>
    <dcat:keyword>sidewash</dcat:keyword>
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    <dct:description>&lt;p&gt;An analysis is described of side-force and yawing-moment-in-sideslip of conventional transport aircraft based on available wind tunnel and full-size aircraft data. After a chapter on general design requirements the analysis is divided in a part which describes the tail-off characteristics and a part which describes the contribution of the tail surfaces to side-force and yawing-moment-due-to-sideslip. Particular attention is paid to the drfferent contributions to the sidewash as expenenced by the tail surfaces. Also rudder characteristics are discussed.&lt;/p&gt;</dct:description>
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