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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    Title :

    Continuous Wound Toroidal Aircraft Tire


    Contributors:

    Publication date :

    1973


    Size :

    34 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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