Blade pressure loading and torque measurement in a transonic linear cascade
XXVI BIENNIAL SYMPOSIUM ON MEASURING TECHNIQUES IN TURBOMACHINERY, MTT2622(2023)
Abstract
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.
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Key words
transonic linear cascade,torque measurement,blade
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