Testing of T-38A landing gear extension at high speed and high altitude is described. The mechanisms are shown together with peak hydraulic pressure data during landing gear deployment with active and inactive strut door flaps. Results of strain gage measurements of stress on various structural members are included.


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    Titel :

    High-Speed T-38A Landing Gear Extension Loads


    Beteiligte:
    A. L. Schmitt (Autor:in)

    Erscheinungsdatum :

    1980


    Format / Umfang :

    17 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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