Axial and circumferential segmented combustor liners for turbojet engine


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    Title :

    Development of a turbojet combustor with a segmentally constructed liner Final summary report


    Contributors:
    Biondi, D. (author) / Draizen, S. (author)

    Publication date :

    1968-06-24


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English