Wing structures containing fuel cells can suffer extensive damage, whereas fuselage and personnel may be relatively unharmed; promising solution lies in development of flexible bladder tanks which will possess sufficient strength and energy absorbing qualities to resist rupture after surrounding structure has failed; fuel tank location.


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    Titel :

    Investigation of crash-fire problems in transport aircraft fuel tanks


    Weitere Titelangaben:

    U S Civ Aeronautics Administration -- Tech Development Report


    Beteiligte:
    Field, R.L. (Autor:in) / Miller, M.F. (Autor:in) / Pigman, G.L. (Autor:in)


    Erscheinungsdatum :

    1951


    Format / Umfang :

    21 pages


    Anmerkungen:

    Illustrations


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Hydrogen fuel tanks for subsonic transport aircraft

    Verstraete, D. / Hendrick, P. / Pilidis, P. et al. | Tema Archiv | 2010


    NACA aircraft crash fire tests

    Pinkel, I.I. / Preston, G.M. / Pesman, G.J. | Engineering Index Backfile | 1953


    Aluminum aircraft fuel tanks

    Dix, Jr., E.H. / Mears, R.B. | Engineering Index Backfile | 1940