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Stall Inception in Axial Flow Compressors
Journal of Turbomachinery, 1991Studies have been conducted on two laboratory test compressors to investigate the process leading to the formation of finite amplitude rotating stall cells. The measurements were obtained from circumferential arrays of hot wires and were spatially and temporarily analyzed to show that modal perturbations are not always present prior to stall, and when ...
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An Improved Axial Flow Compressor Design
The Journal of the Royal Aeronautical Society, 1965In using the method of stage stacking to compute the off-design performance of multi-stage axial compressors, it has been observed that the limitation on performance at speeds above the design speed has been set by the stall and the choke points of the rear stages(1).
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Unsteady Flow in Axial Flow Compressors
1991A review is made of the experimental rotating stall work on a low-speed compressor stage. The instantaneous flow field inside the cell is explored using multiple hot wires in the absolute frame of reference. Rotor blade stall and radial drift of the boundary layer is investigated by on-rotor blade instrumentation.
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Axial-Flow Compressors for Gas Turbines
Journal of Fluids Engineering, 1948Abstract The development of the gas turbine during the last decade has opened a new field for compressor application. The compressor is an essential component of every gas-turbine power plant. It delivers air at some elevated pressure to the burner in sufficient quantity to maintain an efficient combustion of fuel and to cool the ...
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Journal of the Society of Mechanical Engineers, 1967
Syojiro KAJI, Takuro OKAZAKI
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Syojiro KAJI, Takuro OKAZAKI
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A-to-Z Guide to Thermodynamics, Heat and Mass Transfer, and Fluids Engineering, 2006
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Axial flow compressor performance deterioration
20th Joint Propulsion Conference, 1984C. BALAN, W. TABAKOFF
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