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    An experimental investigation of compressor stall using an on-line distortion indicator and signal conditioner (1975)
    In:  CASI
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    Publication Date: 2019-06-27
    Description: The relation of the steady-state and dynamic distortions and the stall margin of a J85-13 turbojet engine was investigated. A distortion indicator capable of computing two distortion indices was used. A special purpose signal conditioner was also used as an interface between transducer signals and distortion indicator. A good correlation of steady-state distortion and stall margin was established. The prediction of stall by using the indices as instantaneous distortion indicators was not successful. A sensitivity factor that related the loss of stall margin to the turbulence level was found.
    Keywords: AERONAUTICS (GENERAL)
    Type: NASA-TM-X-3182 , E-8120
    Format: application/pdf
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