The results of the final analyses which were conducted using a revised structural simulation of the Decoupler Pylon are reported in this addendum. The simulation incorporates the previously published results of ground tests performed on the flight Decoupler Pylons mounted in a test fixture at General Dynamic's Fort Worth facility. The analyses show that the Decoupler Pylon will suppress wing-store flutter for the GBU-8 flight test stores configuration on an F-16 airplane. The feasibility of carrying a B-61 on the pylons is also investigated with the conclusion that the pylons would need to be modified in order to demonstrate flutter suppression. The results of a ground vibration test performed on the 1/4 scale F-16 flutter model and a wind tunnel test with this model and a model Decoupler Pylon are given.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Design and Fabrication of the NASA (National Aeronautics and Space Administration) Decoupler Pylon for the F-16 Aircraft, Addendum 1


    Beteiligte:
    J. D. Clayton (Autor:in) / R. L. Haller (Autor:in)

    Erscheinungsdatum :

    1985


    Format / Umfang :

    70 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Design and Fabrication of the NASA Decoupler Pylon for the F-16 Aircraft

    Clayton, J. D. / Haller, R. L. / Hassler, J. M., Jr. | NTRS | 1985


    Design and Fabrication of the NASA Decoupler Pylon for the F-16 Aircraft

    J. D. Clayton / R. L. Haller / J. M. Hassler | NTIS | 1985