The purpose of this report is to document progress to date on the structural design effort conducted by the Preliminary Design Group, Advanced Structures Branch, Structures Division, in support of a Prototype Division VISTOL Aircraft. The investigation of the use of the Cold Thrust Augmentation (CTA) principle on a VISTOL aircraft was limited to two Prototype Division generated configurations. One configuration involved a CTA pod located at the wing tip while the second configuration was a fuselage mounted CTA system.


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    Title :

    Structural Design Considerations for Cold Thrust Augmentation Fighter Concepts


    Contributors:
    J. D. Oetting (author) / A. Gonsiska (author)

    Publication date :

    1973


    Size :

    29 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English