Unsteady Pressure Measurements in a Heated Rotating Cavity

نویسندگان

چکیده

Abstract The flow in the heated rotating cavity of an aero-engine compressor is driven by buoyancy forces, which result pairs cyclonic and anticyclonic vortices. resultant field three-dimensional, unsteady, unstable, makes it challenging to model heat transfer. In this paper, properties vortex structures are determined from novel unsteady pressure measurements collected on disk surface over a range engine-representative parameters. These first their kind with practical significance engine designer for validation computational fluid dynamics. One cyclonic/anticyclonic pair was detected experimental range, despite measurement harmonic modes frequency spectra at low Rossby numbers. It shown that these were caused unequal size vortices, larger pair. slipped relative disks speed typically around 10%–15% rotor, but precession often unsteady. coherency, strength, slip increased parameter, due stronger they largely independent rotational Reynolds number.

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ژورنال

عنوان ژورنال: Journal of engineering for gas turbines and power

سال: 2022

ISSN: ['0742-4795', '1528-8919']

DOI: https://doi.org/10.1115/1.4053390