Two NASTRAN models of the Gates Learjet Corporation Model 35/36 Wing were developed. The models and the problems encountered in their development are discussed. A skin buckling analysis used for the ultimate loading conditions is presented. A discussion of the static tests and the correlation of the static test with the NASTRAN results and the results of a supplementary semimonocoque beam analysis are also included.


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    Titel :

    Analysis of the Learjet 35/36 Wing and Correlation with Experimental Results


    Beteiligte:
    Abla, M. H. (Autor:in) / Boroughs, R. R. (Autor:in) / Cook, E. L. (Autor:in)


    Erscheinungsdatum :

    1976-10-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



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