Experimental Investigation of Dynamic Stall on a Pitching Rotor Blade Tip

被引：3

作者：

Merz, Christoph B. ^{[1
]}

Wolf, C. Christian ^{[1
]}

Richter, Kai ^{[1
]}

Kaufmann, Kurt ^{[1
]}

Raffel, Markus ^{[1
]}

机构：

[1] German Aerosp Ctr DLR, Inst Aerodynam & Flow Technol, Bunsenstr 10, D-37073 Gottingen, Germany

来源：

NEW RESULTS IN NUMERICAL AND EXPERIMENTAL FLUID MECHANICS X | 2016年 / 132卷

关键词：

D O I：

10.1007/978-3-319-27279-5_30

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

Measurements on a pitching finite rotor blade tip are performed. Sectional forces obtained from surface pressure measurements show a significant difference in maximum loads and the extent of hystereses between a section near the parabolic blade tip and two sections further inboard. Different characteristics appear also in the flow topology over the suction side of the airfoil investigated by means of Particle Image Velocimetry (PIV) at these locations.

引用

页码：339 / 348

页数：10

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