VORTEX BREAKDOWN OVER A PITCHING DELTA-WING

被引：19

作者：

GURSUL, I

YANG, H

机构：

[1] Department of Mechanical, Industrial and Nuclear Engineering, University of Cincinnati, Cincinnati

来源：

JOURNAL OF FLUIDS AND STRUCTURES | 1995年 / 9卷 / 05期

关键词：

D O I：

10.1006/jfls.1995.1032

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 [机械工程];

摘要：

Unsteady pressure measurements were carried out on a pitching delta wing in order to study the effects of pressure gradient on the phase lag between the wing motion and the movement of breakdown location. The results indicate that the observed time lag of breakdown location is strongly linked to the external pressure gradient generated by the wing. (C) 1995 Academic Press Limited

引用

页码：571 / 583

页数：13

共 15 条

[1]

SURVEY OF RESEARCH ON UNSTEADY AERODYNAMIC LOADING OF DELTA WINGS [J].