Finite element analysis of critical stress distribution in canopy of deployed twin keel parawing, predicting failure stress levels


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    Title :

    Structural analysis of a parawing during deployment


    Contributors:

    Conference:

    AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AERODYNAMIC DECELERATION SYSTEMS CONFERENCE ; 1970 ; DAYTON, OH


    Publication date :

    1970-09-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :






    Parawing aerodynamics

    Sleeman, Jr., W.C. / Johnson, Jr., J.L. | Engineering Index Backfile | 1963