Abstract
This paper includes new experimental data on the torsional stability of a compressor or fan type of blade row. This data is linked in with published material to form a three dimensional figure describing the stability of such rows. The data is then discussed by considering relative values of influence coefficients and some of the trends in the stability figure are explained. New data is also included on the relative magnitudes and phases of the influence coefficients.
Original language | English |
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Journal | American Society of Mechanical Engineers (Paper) |
Publication status | Published - 1991 |
Event | International Gas Turbine and Aeroengine Congress and Exposition - Orlando, FL, USA Duration: 3 Jun 1991 → 6 Jun 1991 |