Low-speed Wind-tunnel Test Results of a BWB-UCAV Model

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dc.contributor.authorShim, HoJoonko
dc.contributor.authorPark, Seung Oko
dc.date.accessioned2015-11-20T12:42:14Z-
dc.date.available2015-11-20T12:42:14Z-
dc.date.created2014-01-13-
dc.date.created2014-01-13-
dc.date.issued2013-
dc.identifier.citationProcedia Engineering, v.67, pp.50 - 58-
dc.identifier.issn1877-7058-
dc.identifier.urihttp://hdl.handle.net/10203/201649-
dc.description.abstractWind-tunnel test results of a BWB-UCAV model which was modified slightly from UCAV 1303 at a free stream speed of 50m/s at various angles of attack and yaw angles are presented in the present paper. The six-component force and moment coefficients were measured by using internal balance. Well known pitch-break phenomenon was identified to occur at a rather low angle of attack. Yawing and rolling moment coefficients from the measurements data also were found to exhibit very irregular pitch-break type behavior at non-zero yaw angles. To elucidate some aerodynamic flow structures, surface oil flow visualization and PSP measurements were also carried out.-
dc.languageEnglish-
dc.publisherELSEVIER-
dc.titleLow-speed Wind-tunnel Test Results of a BWB-UCAV Model-
dc.typeArticle-
dc.type.rimsART-
dc.citation.volume67-
dc.citation.beginningpage50-
dc.citation.endingpage58-
dc.citation.publicationnameProcedia Engineering-
dc.identifier.doi10.1016/j.proeng.2013.12.004-
dc.contributor.localauthorPark, Seung O-
dc.contributor.nonIdAuthorShim, HoJoon-
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AE-Journal Papers(저널논문)
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