Blade pressure loading and torque measurement in a transonic linear cascade

被引：0

作者：

Lepicovsky, Jan ^{[1
]}

Simurda, David ^{[1
]}

Hala, Jindrich ^{[1
]}

Sidlof, Petr ^{[2
]}

Stepan, Martin ^{[2
]}

机构：

[1] Czech Acad Sci, Inst Thermomech, Dolejskova 5, Prague, Czech Republic

[2] Tech Univ Liberec, Studentska 2, Liberec, Czech Republic

来源：

XXVI BIENNIAL SYMPOSIUM ON MEASURING TECHNIQUES IN TURBOMACHINERY, MTT2622 | 2023年 / 2511卷

关键词：

D O I：

10.1088/1742-6596/2511/1/012030

中图分类号：

O414.1 [热力学];

学科分类号：

摘要：

Experimental results of a transonic compressor blade pressure loadings and blade shaft torque measurements are presented in this paper. Data were acquired for the cascade middle blade being set to a number of incidence angle offsets to simulate phases of a blade flutter oscillatory motion. This paper should be viewed as a progress report on the ongoing larger research effort on blade flutter in transonic flow regimes.

引用

页数：8

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