COMPARISON OF SUPERCRITICAL AIRFOIL FLOW CALCULATIONS WITH WIND-TUNNEL RESULTS

被引：0

作者：

KING, LS

JOHNSON, DA

机构：

[1] NASA, Ames Research Cent, Moffett, Field, CA, USA, NASA, Ames Research Cent, Moffett Field, CA, USA

来源：

AIAA JOURNAL | 1985年 / 23卷 / 09期

关键词：

D O I：

10.2514/3.9085

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：1301 / 1307

页数：7

共 50 条

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[7] Numerical study of wind-tunnel walls effects on transonic airfoil flow
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[J]. AIAA JOURNAL, 2003, 41 (06) : 1046 - 1054
[8] Numerical study of wind-tunnel walls effects on transonic airfoil flow
[J]. Garbaruk, A, 1600, American Inst. Aeronautics and Astronautics Inc. (41):
[9] NOTE ON TRANSONIC FLOW PAST A THIN AIRFOIL OSCILLATING IN A WIND-TUNNEL
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[J]. JOURNAL OF SOUND AND VIBRATION, 1976, 46 (02) : 195 - 207
[10] Wind-tunnel tests of synthetic jet control effects on airfoil flow separation
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[J]. SCIENTIFIC REPORTS, 2022, 12 (01)

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