DC Field | Value | Language |
---|---|---|
dc.contributor.author | Lee, Sungmin | ko |
dc.contributor.author | Song, Hakyoon | ko |
dc.contributor.author | Park, Gisu | ko |
dc.date.accessioned | 2020-04-14T08:20:05Z | - |
dc.date.available | 2020-04-14T08:20:05Z | - |
dc.date.created | 2020-02-16 | - |
dc.date.created | 2020-02-16 | - |
dc.date.created | 2020-02-16 | - |
dc.date.issued | 2020-03 | - |
dc.identifier.citation | EXPERIMENTS IN FLUIDS, v.61, no.4 | - |
dc.identifier.issn | 0723-4864 | - |
dc.identifier.uri | http://hdl.handle.net/10203/273892 | - |
dc.description.abstract | Strut-support interference effects were investigated at a nominal Mach number of 6. Cylinder and rhombus models are used; moreover, models called half shock-bump (SB) and SB applied to the front and both sides of the shock-bump shape are used. This is beneficial for free-stream flow recovery around the model surface by bumping the compression and expansion waves at a unit Reynolds number of approximately 17.8 x 103/m and a total enthalpy of approximately 1.9 MJ/kg. A quantitative density field analysis is conducted using the background-oriented schlieren technique, which is validated by measuring the shock stand-off distance and density increase rate on a hemisphere model. In this study, flow interference is divided into the measurements of the recompression shock zone thickness as a wake interference and the free-stream flow density recovery beyond the oblique shock as a strut interference. In the SB model, the thickness of the recompression shock zone is approximately 4.4 +/- 0.2 mm, which is a reduction of approximately 53% compared with the cylinder model. In the oblique shock wave height measurements, defined by measuring the intersection of the increasing and decreasing points of density, the SB model shows a height of 16.4 mm, which is approximately 33.6% less than the 24.7 mm height of the cylinder model. In addition, the free-stream flow density beyond the oblique shock wave in the SB model is found to have an approximately 10% deviation from the free-stream density of 0.016 kg/m3, which is more effective than the 106% higher value in the cylinder model. Through such studies of flow interference, the effect of the SB shape on the strut-support is verified. | - |
dc.language | English | - |
dc.publisher | SPRINGER | - |
dc.title | Study of Strut Interference in High-Speed Flows | - |
dc.type | Article | - |
dc.identifier.wosid | 000522022100004 | - |
dc.identifier.scopusid | 2-s2.0-85082516708 | - |
dc.type.rims | ART | - |
dc.citation.volume | 61 | - |
dc.citation.issue | 4 | - |
dc.citation.publicationname | EXPERIMENTS IN FLUIDS | - |
dc.identifier.doi | 10.1007/s00348-020-2934-8 | - |
dc.contributor.localauthor | Park, Gisu | - |
dc.contributor.nonIdAuthor | Lee, Sungmin | - |
dc.contributor.nonIdAuthor | Song, Hakyoon | - |
dc.description.isOpenAccess | N | - |
dc.type.journalArticle | Article | - |
dc.subject.keywordPlus | ALTITUDE ENVIRONMENT SIMULATION | - |
dc.subject.keywordPlus | OXYGEN CATALYTIC RECOMBINATION | - |
dc.subject.keywordPlus | SPACE LAUNCH VEHICLE | - |
dc.subject.keywordPlus | DENSITY-MEASUREMENTS | - |
dc.subject.keywordPlus | SHOCK CONTROL | - |
dc.subject.keywordPlus | COPPER-OXIDE | - |
dc.subject.keywordPlus | SCHLIEREN | - |
dc.subject.keywordPlus | JUNCTION | - |
dc.subject.keywordPlus | SURFACE | - |
dc.subject.keywordPlus | DESIGN | - |
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.