DC Field | Value | Language |
---|---|---|
dc.contributor.author | Na, Hyoung Jin | ko |
dc.contributor.author | Kim, Chun-Gon | ko |
dc.contributor.author | Lee, In | ko |
dc.contributor.author | Kim, Jung-Young | ko |
dc.contributor.author | Bae, Su-Bin | ko |
dc.date.accessioned | 2017-10-23T01:55:28Z | - |
dc.date.available | 2017-10-23T01:55:28Z | - |
dc.date.created | 2017-10-10 | - |
dc.date.created | 2017-10-10 | - |
dc.date.issued | 2017-09 | - |
dc.identifier.citation | JOURNAL OF SPACECRAFT AND ROCKETS, v.54, no.5, pp.1041 - 1049 | - |
dc.identifier.issn | 0022-4650 | - |
dc.identifier.uri | http://hdl.handle.net/10203/226404 | - |
dc.description.abstract | The nonlinear aeroelastic characteristics of a rolling wraparound fin with freeplay nonlinearity are investigated. The aerodynamic forces are computed by solving the Euler equations in a body-fixed rotating coordinate frame. The nonlinear static and normal mode analyses for a rotating wraparound fin are performed using MSC Nastran. The V-g method, the traditional incremental damping approach to compute the flutter velocity, is used for aeroelastic analysis in the frequency domain, and the results are shown to compare with the time-history responses obtained by integration of the equations of motion using minimum state approximation time-domain aerodynamics. The effects of the freeplay nonlinearity and rolling motion of a wraparound fin on aeroelastic characteristics are investigated. | - |
dc.language | English | - |
dc.publisher | AMER INST AERONAUTICS ASTRONAUTICS | - |
dc.subject | MISSILE CONTROL FIN | - |
dc.subject | FLUTTER CHARACTERISTICS | - |
dc.subject | CONTROL SURFACE | - |
dc.subject | FREE PLAY | - |
dc.subject | STRUCTURAL NONLINEARITIES | - |
dc.subject | PROJECTILE | - |
dc.title | Nonlinear Aeroelastic Analysis of a Rolling Wraparound Fin | - |
dc.type | Article | - |
dc.identifier.wosid | 000411061100006 | - |
dc.identifier.scopusid | 2-s2.0-85029719638 | - |
dc.type.rims | ART | - |
dc.citation.volume | 54 | - |
dc.citation.issue | 5 | - |
dc.citation.beginningpage | 1041 | - |
dc.citation.endingpage | 1049 | - |
dc.citation.publicationname | JOURNAL OF SPACECRAFT AND ROCKETS | - |
dc.identifier.doi | 10.2514/1.A33516 | - |
dc.contributor.localauthor | Kim, Chun-Gon | - |
dc.contributor.localauthor | Lee, In | - |
dc.contributor.nonIdAuthor | Kim, Jung-Young | - |
dc.contributor.nonIdAuthor | Bae, Su-Bin | - |
dc.description.isOpenAccess | N | - |
dc.type.journalArticle | Article | - |
dc.subject.keywordPlus | MISSILE CONTROL FIN | - |
dc.subject.keywordPlus | FLUTTER CHARACTERISTICS | - |
dc.subject.keywordPlus | CONTROL SURFACE | - |
dc.subject.keywordPlus | FREE PLAY | - |
dc.subject.keywordPlus | STRUCTURAL NONLINEARITIES | - |
dc.subject.keywordPlus | PROJECTILE | - |
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