Simulated hailstone tests on windshield materials, on nonmetallic materials used in constructing radar housing in nose of airplane fuselage, on metallic leading edge of wings, and on propeller dome; compressed air catapult projects ice spheres ranging from 0.75 to 1.88 in. in diam, at velocities up to 804 mph.


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    Titel :

    Hailstone impact tests on aircraft structural components


    Weitere Titelangaben:

    U S Civ Aeronautics Administration -- Tech Development Report


    Beteiligte:
    Kangas, P. (Autor:in)


    Erscheinungsdatum :

    1950


    Format / Umfang :

    20 pages


    Anmerkungen:

    Illustrations, Diagrams, Charts, Tables


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Hailstone impact simulator

    ALFARO-BOU, E. | AIAA | 1972


    Hailstone impact simulator.

    Alfaro-Bou, E. | NTRS | 1972



    Development of a Hailstone Substitute for Representative Impact Tests

    Deconinck, Paul | British Library Conference Proceedings | 2019


    Modeling hailstone fragmentation upon impact with curved aircraft panels using a modified Hertzian contact mechanics framework

    Pai, Anand / Sowmya, P. K. / Chaudhary, Khushhali et al. | Springer Verlag | 2025

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