Tests at Langley landing-loads track to obtain friction coefficients developed during braking and landing were made at forward speeds of 85 knots with static vertical loads of 20,405 and 13,020 lb; results indicated effect of each type of mat and membrane on variation of coefficient of friction; braking tests for both dry and wet surface conditions.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Braking and landing tests on some new types of airplane landing mats and membranes


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1959


    Size :

    41 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



    Development of airplane landing mats

    Tolbert, R.L. | Engineering Index Backfile | 1945


    Development of airplane landing mats

    Tolbert, R.L. | Engineering Index Backfile | 1945


    Steel landing mats for airplane runways

    Greulich, G.G. | Engineering Index Backfile | 1943


    Steel landing mats for airplane runways

    Greulich, G.G. | Engineering Index Backfile | 1943