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    Unknown
    In:  CASI
    Publication Date: 2019-08-27
    Description: The present work discusses the results of some experimental studies on the possibility of attenuating shock waves in a supersonic flow. The shock waves were formed by an external source of electrical energy. An electromechanical method is described that permits partial recovery of the expended energy.
    Keywords: AERODYNAMICS
    Type: NASA-TM-77912 , NAS 1.15:77912
    Format: application/pdf
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