The data presented in the report were obtained on F-106A S/N 56-455. Data were obtained during normal takeoffs and landings, throughout the level flight regime and under maneuvering conditions involving 2 g turns while decelerating through Mach 1. All flight data were obtained with the aircraft in a clean configuration. It is recommended that the data be used as a basis for preparation of vibration qualification specifications applicable to new aircraft with configurations generally similar to the F-106A/B. (Author)


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    Title :

    F-106A Environmental Vibration


    Contributors:

    Publication date :

    1960


    Size :

    15 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English