The primary objective of the program was to establish basic design requirements for a toroidal continuous wound aircraft tire concept. Using these basic design requirements, tires were fabricated and shipped to the Flight Dynamics Laboratory at WPAFB for their evaluation so as to aid in determining the performance characteristics of the toroidal tire concept on military aircraft applications. (Author)


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    Titel :

    Continuous Wound Toroidal Aircraft Tire


    Beteiligte:

    Erscheinungsdatum :

    1973


    Format / Umfang :

    34 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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