IN the design of scmi-monocoque aircraft structures it is generally assumed that, if failure occurs, it will take place by a collapse of the longitudinal stiffeners between the intermediate frames. This assumption has given reasonable results in the past and has undoubtedly been justified when applied to structures of small and medium size. It is well known that most of the intermediate frames in such structures are of “minimum” sizes, determined by practical considerations.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Semi-Monocoque Cylinders


    Subtitle :

    A Simple Method of Ascertaining the Stability Criterion


    Published in:

    Publication date :

    1938-06-01


    Size :

    2 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    MONOCOQUE AND SEMI-MONOCOQUE PASSENGER SEATS WITH ERGONOMIC DESIGN

    LE NGUYEN TIEN PHUC / MANSOURI REZA / PARKER C MICHAEL et al. | European Patent Office | 2017

    Free access

    MONOCOQUE AND SEMI-MONOCOQUE PASSENGER SEATS WITH ERGONOMIC DESIGN

    LE NGUYEN TIEN PHUC / MANSOURI REZA / PARKER C MICHAEL et al. | European Patent Office | 2016

    Free access

    MONOCOQUE AND SEMI-MONOCOQUE PASSENGER SEATS WITH ERGONOMIC DESIGN

    LE NGUYEN TIEN PHUC / MANSOURI REZA / PARKER C MICHAEL et al. | European Patent Office | 2020

    Free access

    Monocoque and semi-monocoque passenger seats with ergonomic design

    LE NGUYEN TIEN PHUC / MANSOURI REZA / PARKER C MICHAEL et al. | European Patent Office | 2023

    Free access

    MONOCOQUE AND SEMI-MONOCOQUE PASSENGER SEATS WITH ERGONOMIC DESIGN

    LE NGUYEN TIEN PHUC / MANSOURI REZA / PARKER C MICHAEL et al. | European Patent Office | 2017

    Free access