Low-Frequency Shock Motion in Transonic Convex-Corner Flows

被引：4

作者：

Chung, Kung-Ming ^{[1
]}

Lee, Kuan-Huang ^{[1
]}

Chang, Po-Hsiung ^{[2
]}

机构：

[1] Natl Cheng Kung Univ, Aerosp Sci & Technol Res Ctr, Tainan 711, Taiwan

[2] Natl Univ Singapore, Temasek Labs, Singapore 119077, Singapore

来源：

关键词：

BOUNDARY-LAYER INTERACTIONS; UNSTEADINESS; SEPARATION; OSCILLATIONS; MODEL;

D O I：

10.2514/1.J055430

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

[No abstract available]

引用

页码：2109 / 2112

页数：4

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