Cross-flow Analogy and Euler Solutions for Missile Body Aerodynamics

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dc.contributor.author이재명ko
dc.contributor.author박승오ko
dc.contributor.author김인선ko
dc.date.accessioned2009-12-09T02:03:02Z-
dc.date.available2009-12-09T02:03:02Z-
dc.date.created2012-02-06-
dc.date.created2012-02-06-
dc.date.issued2000-11-
dc.identifier.citationINTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES , v.1, no.2, pp.9 - 16-
dc.identifier.issn2093-274X-
dc.identifier.urihttp://hdl.handle.net/10203/14414-
dc.description.abstractFor aerodynamic design of missile bodies of non-circular cross-section, the combination of the slender body theory and the cross-flow analogy can hardly be applied owing to the lack of experimental data. An alternative is to utilize the Euler solution in the design stage. For enhanced accuracy, however, an adequate viscous correction is necessary to the Euler solution. In this work, such a procedure is examined to compensate the viscous effect by utilizing the concept of proportionality factor in cross-flow analogy. Predictions of aerodynamic coefficients combining the Euler solution and the viscous correction via proportionality factor are made for a missile body of elliptic cross-section. Results indicate that the present approach can be adopted in designing missile bodies of non-circular cross-sections.-
dc.languageKorean-
dc.language.isoen_USen
dc.publisher한국항공우주학회-
dc.titleCross-flow Analogy and Euler Solutions for Missile Body Aerodynamics-
dc.typeArticle-
dc.type.rimsART-
dc.citation.volume1-
dc.citation.issue2-
dc.citation.beginningpage9-
dc.citation.endingpage16-
dc.citation.publicationnameINTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES-
dc.embargo.liftdate9999-12-31-
dc.embargo.terms9999-12-31-
dc.contributor.localauthor박승오-
dc.contributor.nonIdAuthor이재명-
dc.contributor.nonIdAuthor김인선-
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AE-Journal Papers(저널논문)
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