Application of boron laminates in wing extension and pressurized fuel tank for F-111B aircraft; incorporation of boron-epoxy face sheets and full depth honeycomb core is principle method of construction; discussion of material testing method, design of wing extension and configuration of pressurized fuel tank, fabrication techniques and inspection procedures.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Boron wing extension for F-111B aircraft


    Additional title:

    SPE -- Annual Tech Conference


    Contributors:
    Lubin, G. (author) / Ludwig, W. (author) / August, A. (author)

    Conference:

    26th Annual Technical Conference of SPE ; 1968 Plastics



    Publication date :

    1968


    Size :

    10 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English