During October and November 2000 the Naval Air Warfare Center, China Lake conducted a series of simulated uncontained engine failure structural impact tests. A large 12-inch gas gun was used to launch turbojet engine fan blade segments into a narrow-body commercial aircraft fuselage. The impacts were documented and analyzed with high-speed photography. Impact velocities, presented areas, and residual velocities were calculated. These data were then compared to analytic results predicted by the Joint Technical Coordinating Group for Munitions Effectiveness (JTCG/ME) penetration equations. The results are presented in this report.


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    Titel :

    Engine Debris Fuselage Penetration Testing Phase 2


    Beteiligte:
    S. J. Lundin (Autor:in)

    Erscheinungsdatum :

    2002


    Format / Umfang :

    82 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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