An Experimental Investigation of Stator/rotor Interaction Influence on Multistage Compressor Rotor Flow PDF Download
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Author: Daniel Lawrence Tweedt
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 64
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Author: Daniel Lawrence Tweedt
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 64
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Author: Theodore Hisao Okiishi
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 16
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Author: Johannes Schreiber
Publisher:
ISBN:
Category :
Languages : en
Pages : 214
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The following experimental and numerical investigations aim at the deep understanding of the flow field in the 3.5 stages high-speed axial compressor CREATE, studied on a 2 MW test rig at the Laboratory of Fluid Mechanics and Acoustics (LMFA) in Lyon, France. This work focuses on three major objectives: Firstly, a global description of the flow field with an identification of limitations to the used exploration methods; Secondly, the characterization of the effect of stator-stator clocking in a high-speed compressor; Thirdly, the identification of instabilities arising at low mass flow rates for confirming studies on low-speed compressors and giving new insights.This work demonstrates that a mis-interpretation of steady performance data occurs easily due to measurement constraints and correction coefficients are proposed. At certain locations in the compressor, the flow field exploration (experimental and numerical) methods are identified to be challenged. This identification will initiate further development of the methods. The main mis-predictions of the simulations concern the over-prediction of the blockage induced by the tip leakage flow and eventually an over-predicted pressure rise. Furthermore, the measurements provided by the pneumatic pressure probes over-estimate the static pressure upstream of the stators. This error is induced by the interaction between the stator potential field and the probe it-self. In addition, the laser Doppler anemometry method over-estimates the velocity downstream the stators. The transport of the rotor wakes through the stators might not be correctly captured with the seeding particles in this high-speed compressor.The investigation of the stator clocking reveals only a small global effect within the measurement uncertainty band. Several contributions to the weak effect of clocking are identified by analysis of the flow structure transport, namely the time-mean mixing out of the stator wakes and the deformation of wakes along their flow path. The local effect of clocking depends on the span-height because of the variation of the circumferential position of the stator wakes and the stator blade shape over the span-height. Local possible positive and negative effects of clocking are identified and are shown to be almost in balance in this compressor. Furthermore, this work demonstrates that the unsteadiness in the flow field is not linked conclusively to the stator clocking.In this compressor, the arising instabilities depend on the operating point and flow field exploration methods. At stable operating points and nominal compressor speed, the numerical results reveal a rotating disturbance in the rotors 2 and 3, whereas the measurements show a rotating disturbance only in the first rotor and only at part speed. In both cases the disturbance exhibits rotating instability like characteristics. An exhaustive numerical study allows to exclude the commonly assumed influence of rotor-stator interactions on the rotating disturbance and pinpoints its source. New insights into the stable behavior and periodicity of the measured rotating instability are derived contrary to the unstable behavior suggested by the naming and literature. This disturbance is shown to evolve into rotating stall cells when approaching the stability limit. At nominal compressor speed, a spike type surge inception is identified I n the measured field. A precise description of the abrupt onset of the spike cell and its difference to a rotating stall cell are presented.
Author: N. Arndt
Publisher:
ISBN:
Category : Blades
Languages : en
Pages : 0
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Author: Norbert Karl Erhard Arndt
Publisher:
ISBN:
Category : Electronic dissertations
Languages : en
Pages : 420
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Author: T. Zandbergen
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 54
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 548
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Author: Bo Hu
Publisher:
ISBN:
Category : Impact
Languages : en
Pages :
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 654
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Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 804
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