Detailed structural make-up of 4-engine, midwing monoplane; fuselage is semi-monocoque shell consisting of smooth skin reinforced with Z-type 24ST Alclad rolled stiffeners or stringers and transverse bulkheads and belt frames.


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    Title :

    Design analysis of consolidated B-24 liberator


    Additional title:

    Aviation


    Contributors:
    Famme, J.H. (author)

    Published in:

    Aviation ; 44 , n 7 ; p 121-143


    Publication date :

    1945


    Size :

    23 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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