DC Field | Value | Language |
---|---|---|
dc.contributor.author | 윤재건 | ko |
dc.contributor.author | 유지창 | ko |
dc.contributor.author | 이정권 | ko |
dc.date.accessioned | 2013-02-25T19:12:33Z | - |
dc.date.available | 2013-02-25T19:12:33Z | - |
dc.date.created | 2012-02-06 | - |
dc.date.created | 2012-02-06 | - |
dc.date.created | 2012-02-06 | - |
dc.date.issued | 1994-01 | - |
dc.identifier.citation | TRANSACTIONS OF THE KOREAN SOCIETY OF MECHANICAL ENG., v.18, no.4, pp.1081 - 1086 | - |
dc.identifier.issn | 1226-4873 | - |
dc.identifier.uri | http://hdl.handle.net/10203/64589 | - |
dc.description.abstract | The phenomena called "combustion instabilities" in a solid-propellant rocket motor may be viewed as sustaining or amplifying pressure waves. Energy is supplied by combustion processes near the surface of the burning propellant. T-burner method is used to determine the response function of the propellant to the pressure wave. But initial tests were failed because of the Helmholtz resonation inside the T-burner. Acoustic analysis of the original T-burner is carried out and suppression techniques for the Helmholtz oscillation are introduced.ntroduced | - |
dc.language | Korean | - |
dc.publisher | 대한기계학회 | - |
dc.title | 고체추진제의 연소불안정 특성 측정방법에 대한 연구 | - |
dc.title.alternative | A Study on Determining Method of Combustion Instability Characteristics of Solid Propellants | - |
dc.type | Article | - |
dc.type.rims | ART | - |
dc.citation.volume | 18 | - |
dc.citation.issue | 4 | - |
dc.citation.beginningpage | 1081 | - |
dc.citation.endingpage | 1086 | - |
dc.citation.publicationname | TRANSACTIONS OF THE KOREAN SOCIETY OF MECHANICAL ENG. | - |
dc.contributor.localauthor | 이정권 | - |
dc.contributor.nonIdAuthor | 윤재건 | - |
dc.contributor.nonIdAuthor | 유지창 | - |
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