The report describes a study conducted to develop CBR design curves for an aluminum landing mat. The design curves were to represent 1600 operational cycles of an aircraft having a 60,000-lb gross weight with a single-wheel main gear assembly load of 27,000 lb and a 30-7.7 tire inflated to 400 psi. CBR design curves were also desired for 1600 passes of a 39,000-lb single-wheel load applied in a single track to represent the calculated loading imposed on the landing mat during launching of the 60,000-lb aircraft by catapult. (Author)


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    Title :

    Development of CBR Design Curves for Harvey Aluminum Landing Mat


    Publication date :

    1964


    Size :

    52 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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