The structural development work performed on the Learjet 28/29 wing using NASTRAN analysis is discussed. The work included the basic sizing of primary structural members such as wing skins, wing skin splices, and spar caps, as well as the calculation of preliminary weight estimates utilizing the weight computation routine in NASTRAN. The eight spar redundancy of the Learjet wing made this task somewhat more complex than for more determinate type wing structures. Some of the problems that were encountered and the solutions and methods that were used are described.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Development of the Learjet 28/29 Wing Using NASTRAN Analysis


    Contributors:


    Publication date :

    1980-05-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English





    Aerodynamic Tailoring of the Learjet Model 60 Wing

    Chandrasekharan, R. M. / Hawke, V. M. / Hinson, M. L. et al. | British Library Conference Proceedings | 1993


    Aerodynamic tailoring of the Learjet Model 60 wing

    Chandrasekharan, Reuben M. / Hawke, Veronica M. / Hinson, Michael L. et al. | NTRS | 1993


    Aerodynamic Tailoring of the Learjet Model 60 Wing

    Madson, Michael D. / Hinson, Michael L. / Chandrasekharan, Reuben M. et al. | SAE | 1993


    Analysis: Learjet 40

    George, F. | British Library Online Contents | 2004