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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    High-speed T-38A landing gear extension loads


    Contributors:

    Publication date :

    1980-03-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






    Operational Loads on Landing Gear

    Ladda, V. / Struck, H. / North Atlantic Treaty Organization; Advisory Group for Aerospace Research and Development; Structures and Materials Panel | British Library Conference Proceedings | 1991


    Operational Loads on Landing Gear

    V. Ladda / H. Struck | NTIS | 1990


    Landing Gear Retraction Under Aerodynamic Loads

    Duda, Benjamin M. / Deuring, Andreas / Flores Alvarenga, Francisco et al. | AIAA | 2022