Overhead projections are presented. Thrust vectoring and deflection principles are examined with the examples of American and Russian military aircraft such as the F-14, X-31, and YAK-38. Curves on pitch and yaw deflection distribution are presented. Thrust vectoring systems were depicted in aircraft and ground tests. Vane temperature of vibration results were obtained. Curves of thrust moment versus aerodynamic moment were studied, and it is concluded that the thrust generated moment must be used at low Mach/dynamic pressure. Axisymmetric thrust vectoring potential utilization and trim requirements were examined. New aircraft concepts were proposed, with emphasis on elimination or reduction of tails. It is pointed out that thrust vectoring augmentation improves aircraft performances and weapon system modifications are necessary to exploit aircraft performance increases.


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    Title :

    Hochleistungsflugzeuge MIT Schubvektorsteuerung (Advanced Aircraft with Thrust Vector Control)


    Contributors:
    H. Ross (author)

    Publication date :

    1992


    Size :

    110 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English