EXPERIMENTS ON THE AUTOMATIC-CONTROL OF BOUNDARY-LAYER-TRANSITION

被引：12

作者：

RIOUAL, JL

NELSON, PA

FISHER, MJ

机构：

[1] University of Southampton, Fluid Dynamics and Acoustics Group, Institute of Sound and Vibration Research, Highfield, Southampton

来源：

JOURNAL OF AIRCRAFT | 1994年 / 31卷 / 06期

关键词：

Control equipment - Flow control - Position control - Pressure drop - System stability - Transition flow - Wind tunnels;

D O I：

10.2514/3.46668

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：1416 / 1418

页数：3

共 9 条

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[2]

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[3]

Reynolds G.A., Saric W.S., Experiments on the stability of the flat-plate boundary layer with suction, Alaa Journal, 24, 2, pp. 202-207, (1986)

[4]

Arnal D., Boundary Layer Transition, Prediction, Application to Drag Reduction, pp. 1-5, (1992)

[5]

Gedney C.J., Leehey P., Wall pressure fluctuations during transition on a flat plate, Journal of Vibration and Acoustics, 113, (1991)

[6]

Schubauer G.B., Klebanoff P.S., Contribution on the Mechanics of Boundary Layer Transition, (1956)

[7]

Wellstead P.E., Zarrop M.B., Self-Tuning Systems, pp. 71-116, (1991)

[8]

Richards R.J., An Introduction to Dynamics and Control, pp. 165-218, (1979)

[9]

Nelson P.A., Rioual J.-L., Fisher M.J., Experiments on the Active Control of Boundary Layer Transition, pp. 56-62, (1992)