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    Analysis of the Learjet 35/36 Wing and Correlation with Experimental Results (1976)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Description: 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.
    Keywords: STRUCTURAL MECHANICS
    Type: NASA. Ames Res. Center NASTRAN: User's Experiences; p 331-352
    Format: application/pdf
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