Blade pressure loading and torque measurement in a transonic linear cascade

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F61388998%3A_____%2F23%3A00573638" target="_blank" >RIV/61388998:_____/23:00573638 - isvavai.cz</a>
Alternative codes found
RIV/46747885:24220/23:00012228
Result on the web
<a href="https://iopscience.iop.org/article/10.1088/1742-6596/2511/1/012030/pdf" target="_blank" >https://iopscience.iop.org/article/10.1088/1742-6596/2511/1/012030/pdf</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1088/1742-6596/2511/1/012030" target="_blank" >10.1088/1742-6596/2511/1/012030</a>

Result language
angličtina
Original language name
Blade pressure loading and torque measurement in a transonic linear cascade
Original language description
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.
Czech name
—
Czech description
—

Project
<a href="/en/project/LTAUSA19036" target="_blank" >LTAUSA19036: Advanced experimental research on synchronous and non-synchronous blade vibration</a><br>
Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year
2023
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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