Presentation Open Access
Obert, Ed
<?xml version='1.0' encoding='utf-8'?> <resource xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xmlns="http://datacite.org/schema/kernel-4" xsi:schemaLocation="http://datacite.org/schema/kernel-4 http://schema.datacite.org/meta/kernel-4.1/metadata.xsd"> <identifier identifierType="DOI">10.5281/zenodo.21443</identifier> <creators> <creator> <creatorName>Obert, Ed</creatorName> <givenName>Ed</givenName> <familyName>Obert</familyName> </creator> </creators> <titles> <title>Static Directional Stability and Control of Transport Aircraft</title> </titles> <publisher>Zenodo</publisher> <publicationYear>2013</publicationYear> <subjects> <subject>stability</subject> <subject>static directional stability</subject> <subject>control</subject> <subject>transport</subject> <subject>aircraft</subject> <subject>side force</subject> <subject>yaw</subject> <subject>sideslip</subject> <subject>wind tunnel</subject> <subject>tail</subject> <subject>wing</subject> <subject>sidewash</subject> <subject>rudder</subject> <subject>EWADE2013</subject> </subjects> <dates> <date dateType="Issued">2013-09-18</date> </dates> <resourceType resourceTypeGeneral="Text">Presentation</resourceType> <alternateIdentifiers> <alternateIdentifier alternateIdentifierType="url">https://zenodo.org/record/21443</alternateIdentifier> </alternateIdentifiers> <relatedIdentifiers> <relatedIdentifier relatedIdentifierType="URL" relationType="IsPartOf">https://zenodo.org/communities/ewade</relatedIdentifier> </relatedIdentifiers> <rightsList> <rights rightsURI="https://creativecommons.org/licenses/by/4.0/legalcode">Creative Commons Attribution 4.0 International</rights> <rights rightsURI="info:eu-repo/semantics/openAccess">Open Access</rights> </rightsList> <descriptions> <description descriptionType="Abstract"><p>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.</p></description> <description descriptionType="Other">http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org</description> </descriptions> </resource>
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