Program involving design, development, test, and evaluation of boron-fiber-reinforced airframe component is described; development article is approximate half-scale representation of aircraft structural beam-column scaled to simulate thickness ratio, slenderness ratio, and stress levels of full-sized part under static design conditions; design, manufacturing, and test methods are described, and salient problem areas are discussed. (12253)


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    Title :

    Design and development study of aircraft structural composites


    Additional title:

    Soc Aerospace Matl and Process Engrs Nat Symp


    Contributors:
    Lehman, G.M. (author) / Palmer, R.J. (author)

    Conference:

    12th SAMPE National Symposium -- Advances in Structural Composites ; 1967



    Publication date :

    1967


    Size :

    17 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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