Experimental study of flow around axisymmetric bodies in supersonic flow in case of a local injection into the boundary layer; MATEC Web of Conferences; Vol. 115 : XXXIII Siberian Thermophysical Seminar (STS-33)
| Parent link: | MATEC Web of Conferences Vol. 115 : XXXIII Siberian Thermophysical Seminar (STS-33).— 2017.— [02012, 4 p.] |
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| 団体著者: | |
| その他の著者: | , , , , , , |
| 要約: | Title screen A technique of experimental determination of the parameters and structure of supersonic air flow around of axisymmetric bodies form in the range of Mach numbers M = (2 ч 5) are presented. The results of the investigation of the interaction a supersonic stream flowing around of an axisymmetric model with gas jet which inject into the boundary layer are given. |
| 言語: | 英語 |
| 出版事項: |
2017
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| シリーズ: | Chapter 2 :Turbulent flows, heat and mass transfer in single-phase flows, heat transfer enhancement |
| 主題: | |
| オンライン･アクセス: | https://doi.org/10.1051/matecconf/201711502012 |
| フォーマット: | 電子媒体 図書の章 |
| KOHA link: | https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=655598 |
| 要約: | Title screen A technique of experimental determination of the parameters and structure of supersonic air flow around of axisymmetric bodies form in the range of Mach numbers M = (2 ч 5) are presented. The results of the investigation of the interaction a supersonic stream flowing around of an axisymmetric model with gas jet which inject into the boundary layer are given. |
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| DOI: | 10.1051/matecconf/201711502012 |